LEMUR-2 PEGGY-2004
NORAD 68479
Payload
LEO
2026-067BR
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LEO · NORAD 68479
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Altitude (km)
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Speed (km/s)
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Latitude
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Longitude
🛰️ Orbital Parameters
Perigee
589 km
Apogee
590 km
Inclination
97.8°
Period
96.5 min
Mean Motion
14.92762647 rev/day
TLE Epoch
2026-06-19 15:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude590 km
Orbital Velocity27,243 km/h
Velocity7.57 km/s
Orbital Period96 minutes
Orbits / Day14.93
Eccentricity0.0001
Semi-Major Axis6,961 km
Orbit ClassSun-Synchronous (SSO)
Est. Orbital Lifetime~3–10 years
🚀 Launch & Identity
Country / Operator
Spire Global (Luxembourg)
Launch Date
2026-03-30
Launch Site
Vandenberg SFB, California
Int'l Designator
2026-067BR
Object Type
Payload
RCS Size
Medium (0.1–1 m²)
📖 About This Object
LEMUR-2 PEGGY-2004 is an active satellite operated by Spire Global (Luxembourg), launched on 2026-03-30 from Vandenberg SFB, California. As a relatively recent addition to the catalogue, its orbital elements are well-characterised. It orbits in Low Earth Orbit (LEO) at altitudes between 589 km and 590 km with an inclination of 97.8°. It travels at approximately 27,243 km/h (7.57 km/s), completing one full orbit every 96 minutes — that’s roughly 14.93 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. At its current altitude, the estimated orbital lifetime before atmospheric re-entry is ~3–10 years. Orbital Radar tracks LEMUR-2 PEGGY-2004 in real time using the latest two-line element set (TLE) data, providing live position, altitude, speed and orbital path updated continuously.
🌍 Orbit Context
LEMUR-2 PEGGY-2004 orbits at an average altitude of 590 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 LEMUR-2 PEGGY-2004’s average altitude, there are currently 3,016 active payloads and 603 tracked debris or rocket body fragments — notable neighbours include ONEWEB-0050, STARLINK-3005, STARLINK-3090. This makes it one of the more crowded altitude bands, containing roughly 17.3% of all active satellites. With an inclination of 97.8°, LEMUR-2 PEGGY-2004 passes over latitudes between 97.8°N and 97.8°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. Luxembourg operates approximately 12 active satellites in total, of which 5 share a similar altitude band with LEMUR-2 PEGGY-2004.
🔗 Spire Global Constellation
This satellite is part of Spire Global's constellation of 3U CubeSats collecting weather, maritime and aviation data through radio occultation, AIS and ADS-B payloads. Spire operates over 100 multi-purpose nanosatellites in LEO, providing atmospheric profiles used by weather agencies worldwide, global ship tracking and flight tracking services.
❓ Frequently Asked Questions
LEMUR-2 PEGGY-2004 is in a sun-synchronous orbit (SSO), a specialised form of LEO at approximately 590 km altitude. Its 97.8° 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 96 minutes, travelling at 27,243 km/h.
LEMUR-2 PEGGY-2004 is operated by Spire Global (Luxembourg). It is catalogued by the U.S. Space Surveillance Network under NORAD ID 68479. You can track LEMUR-2 PEGGY-2004 in real time on Orbital Radar’s live tracker or browse all operators in the operator directory.
LEMUR-2 PEGGY-2004 was launched on 2026-03-30 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: ~3–10 years. View the full satellite launch log.
Yes — Orbital Radar tracks LEMUR-2 PEGGY-2004 (NORAD ID 68479) 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.
LEMUR-2 PEGGY-2004 travels at approximately 27,243 km/h (16,928 mph) — roughly 7.57 km/s. It completes 14.93 orbits per day, meaning the crew or instruments aboard (if any) would experience approximately 30 sunrises and sunsets every 24 hours.