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PELICAN-1

NORAD 58296 Payload LEO 2023-174AS ● Active
CONNECTING… LEO · NORAD 58296
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Altitude (km)
Speed (km/s)
Latitude
Longitude
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🛰️ Orbital Parameters
Perigee
350 km
Apogee
351 km
Inclination
97.4°
Period
91.5 min
Mean Motion
15.72813006 rev/day
TLE Epoch
2026-06-19 18:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude351 km
Orbital Velocity27,723 km/h
Velocity7.70 km/s
Orbital Period92 minutes
Orbits / Day15.73
Eccentricity0.0001
Semi-Major Axis6,722 km
Orbit ClassSun-Synchronous (SSO)
Est. Orbital LifetimeMonths to ~1 year
🚀 Launch & Identity
Country / Operator
🇺🇸 Planet Labs (United States)
Launch Date
2023-11-11
Launch Site
Vandenberg SFB, California
Int'l Designator
2023-174AS
Object Type
Payload
RCS Size
Large (>1 m²)
🔗 Constellation / Groups
planet
📖 About This Object
PELICAN-1 is an active satellite operated by Planet Labs (United States), launched on 2023-11-11 from Vandenberg SFB, California. It orbits in Low Earth Orbit (LEO) at altitudes between 350 km and 351 km with an inclination of 97.4°. It travels at approximately 27,723 km/h (7.70 km/s), completing one full orbit every 92 minutes — that’s roughly 15.73 orbits per day. Its near-polar, sun-synchronous orbit means it passes over any given point on Earth at approximately the same local solar time, ideal for consistent Earth observation lighting conditions. Its near-circular orbit (eccentricity close to zero) means it maintains a very consistent altitude throughout each revolution. It is part of the Planet constellation group. At its current altitude, the estimated orbital lifetime before atmospheric re-entry is months to ~1 year. Orbital Radar tracks PELICAN-1 in real time using the latest two-line element set (TLE) data, providing live position, altitude, speed and orbital path updated continuously.
🌍 Orbit Context
PELICAN-1 orbits at an average altitude of 351 km in a sun-synchronous orbit (SSO), a specialised subset of LEO where the orbital plane precesses to maintain a constant angle relative to the Sun. This provides consistent lighting conditions on every pass — essential for Earth observation, weather monitoring and environmental science. Within ±50 km of PELICAN-1’s average altitude, there are currently 1,140 active payloads and 41 tracked debris or rocket body fragments — notable neighbours include STARLINK-1020, STARLINK-1036, STARLINK-1043. This makes it one of the more crowded altitude bands, containing roughly 6.5% of all active satellites. With an inclination of 97.4°, PELICAN-1 passes over latitudes between 97.4°N and 97.4°S, providing near-global coverage including the polar regions. Polar and near-polar orbits are used for reconnaissance, weather monitoring and Earth-observation missions that need to image every part of the planet. United States operates approximately 12,339 active satellites in total, of which 1,058 share a similar altitude band with PELICAN-1.
🔗 Planet Labs Earth Imaging

This satellite is part of Planet Labs' Earth observation fleet — the largest commercial imaging constellation. Planet operates over 200 satellites including Flock (Dove) 3U CubeSats that image the entire landmass daily at 3–5 m resolution and SkySat satellites providing sub-metre imagery and video. The constellation enables change detection, agricultural monitoring, disaster response and environmental analysis at unprecedented temporal resolution.

❓ Frequently Asked Questions
PELICAN-1 is in a sun-synchronous orbit (SSO), a specialised form of LEO at approximately 351 km altitude. Its 97.4° inclination causes the orbital plane to precess at exactly the rate of the Earth’s revolution around the Sun, so the satellite crosses each latitude at a consistent local solar time. It completes one orbit every 92 minutes, travelling at 27,723 km/h.
PELICAN-1 is operated by Planet Labs (United States). It is catalogued by the U.S. Space Surveillance Network under NORAD ID 58296. You can track PELICAN-1 in real time on Orbital Radar’s live tracker or browse all operators in the operator directory.
PELICAN-1 was launched on 2023-11-11 from Vandenberg SFB, California, primarily used for polar and sun-synchronous orbit launches due to its southward ocean trajectory from California. At its current altitude, the estimated remaining orbital lifetime is: months to ~1 year. View the full satellite launch log.
Yes — Orbital Radar tracks PELICAN-1 (NORAD ID 58296) using the latest TLE (two-line element set) data from Space-Track and CelesTrak. Open the live tracker to see its current position, altitude, speed and orbital path updated in real time. You can also browse the satellite directory to find other tracked objects.
PELICAN-1 travels at approximately 27,723 km/h (17,226 mph) — roughly 7.70 km/s. It completes 15.73 orbits per day, meaning the crew or instruments aboard (if any) would experience approximately 31 sunrises and sunsets every 24 hours.
PELICAN-1 is a member of the Planet constellation. Satellites in this group work together to provide coordinated coverage, typically in similar orbital planes at comparable altitudes. You can view all Planet satellites on Orbital Radar’s live tracker.