GNOMES-4
NORAD 58462
Payload
LEO
2023-185A
● Active
CONNECTING…
LEO · NORAD 58462
NOW PASSING OVER
Calculating position…
—
Altitude (km)
—
Speed (km/s)
—
Latitude
—
Longitude
🛰️ Orbital Parameters
Perigee
563 km
Apogee
577 km
Inclination
97.5°
Period
96.1 min
Mean Motion
14.98598147 rev/day
TLE Epoch
2026-11-01 22:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude570 km
Orbital Velocity27,281 km/h
Velocity7.58 km/s
Orbital Period96 minutes
Orbits / Day14.99
Eccentricity0.0010
Semi-Major Axis6,941 km
Orbit ClassSun-Synchronous (SSO)
Est. Orbital Lifetime~3–10 years
🚀 Launch & Identity
Country / Operator
🇺🇸 PLANQ (United States)
Launch Date
2023-12-01
Launch Site
Vandenberg Space Force Base, United States
Int'l Designator
2023-185A
Object Type
Payload
RCS Size
Medium (0.1–1 m²)
📖 About This Object
GNOMES-4 is an active satellite operated by PLANQ (United States), launched on 2023-12-01 from Vandenberg Space Force Base, United States on the Korea 425 launch. It orbits in Low Earth Orbit (LEO) at altitudes between 563 km and 577 km with an inclination of 97.5°. It travels at approximately 27,281 km/h (7.58 km/s), completing one full orbit every 96 minutes — that’s roughly 14.99 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. At its current altitude, the estimated orbital lifetime before atmospheric re-entry is ~3–10 years. Orbital Radar tracks GNOMES-4 in real time using the latest two-line element set (TLE) data, providing live position, altitude, speed and orbital path updated continuously.
🌍 Orbit Context
GNOMES-4 orbits at an average altitude of 570 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 GNOMES-4’s average altitude, there are currently 1,089 active payloads and 533 tracked debris or rocket body fragments — notable neighbours include ONEWEB-0050, STARLINK-3005, STARLINK-3055. This makes it one of the more crowded altitude bands, containing roughly 5.7% of all active satellites. With an inclination of 97.5°, GNOMES-4 passes over latitudes between 97.5°N and 97.5°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 13,340 active satellites in total, of which 491 share a similar altitude band with GNOMES-4.
❓ Frequently Asked Questions
GNOMES-4 is in a sun-synchronous orbit (SSO), a specialised form of LEO at approximately 570 km altitude. Its 97.5° 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 27,281 km/h.
GNOMES-4 is operated by PLANQ (United States). It is catalogued by the U.S. Space Surveillance Network under NORAD ID 58462. You can track GNOMES-4 in real time on Orbital Radar’s live tracker or browse all operators in the operator directory.
GNOMES-4 was launched on 2023-12-01 from Vandenberg Space Force Base, United States, 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 GNOMES-4 (NORAD ID 58462) using the latest TLE (two-line element set) orbital data in its live tracking catalogue (see our data sources). 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.
GNOMES-4 travels at approximately 27,281 km/h (16,952 mph) — roughly 7.58 km/s. It completes 14.99 orbits per day, meaning the crew or instruments aboard (if any) would experience approximately 30 sunrises and sunsets every 24 hours.