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GP-B

NORAD 28230 Payload LEO 2004-014A ● Active
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Altitude (km)
Speed (km/s)
Latitude
Longitude
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🛰️ Orbital Parameters
Perigee
618 km
Apogee
620 km
Inclination
89.8°
Period
97.1 min
Mean Motion
14.83283377 rev/day
TLE Epoch
2026-06-19 04:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude619 km
Orbital Velocity27,185 km/h
Velocity7.55 km/s
Orbital Period97 minutes
Orbits / Day14.83
Eccentricity0.0001
Semi-Major Axis6,990 km
Est. Orbital Lifetime~10–25 years
🚀 Launch & Identity
Country / Operator
🇺🇸 United States
Launch Date
2004-04-20
Launch Site
Vandenberg SFB, California
Int'l Designator
2004-014A
Object Type
Payload
RCS Size
Large (>1 m²)
📖 About This Object
GP-B is an active satellite operated by United States, launched on 2004-04-20 from Vandenberg SFB, California. With over 22 years in orbit, it has far exceeded many satellites’ design lifetimes. It orbits in Low Earth Orbit (LEO) at altitudes between 618 km and 620 km with an inclination of 89.8°. It travels at approximately 27,185 km/h (7.55 km/s), completing one full orbit every 97 minutes — that’s roughly 14.83 orbits per day. 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 ~10–25 years. Orbital Radar tracks GP-B in real time using the latest two-line element set (TLE) data, providing live position, altitude, speed and orbital path updated continuously.
🌍 Orbit Context
GP-B orbits at an average altitude of 619 km in the mid-LEO band, where atmospheric drag is minimal but radiation exposure remains manageable. Objects at this altitude persist for decades to centuries, making debris mitigation critical. This regime is popular for remote sensing constellations and scientific instruments that need stable, long-duration orbits. Within ±50 km of GP-B’s average altitude, there are currently 1,548 active payloads and 761 tracked debris or rocket body fragments — notable neighbours include ONEWEB-0050, STARLINK-3090, STARLINK-3077. This makes it one of the more crowded altitude bands, containing roughly 8.9% of all active satellites. With an inclination of 89.8°, GP-B passes over latitudes between 89.8°N and 89.8°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. United States operates approximately 12,339 active satellites in total, of which 1,060 share a similar altitude band with GP-B.
❓ Frequently Asked Questions
GP-B orbits in Low Earth Orbit (LEO) at altitudes between 618 km (perigee) and 620 km (apogee), with an average altitude of approximately 619 km. It completes one orbit every 97 minutes, travelling at approximately 27,185 km/h (16,892 mph).
GP-B is operated by United States. It is catalogued by the U.S. Space Surveillance Network under NORAD ID 28230. You can track GP-B in real time on Orbital Radar’s live tracker or browse all operators in the operator directory.
GP-B was launched on 2004-04-20 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: ~10–25 years. View the full satellite launch log.
Yes — Orbital Radar tracks GP-B (NORAD ID 28230) 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.
GP-B travels at approximately 27,185 km/h (16,892 mph) — roughly 7.55 km/s. It completes 14.83 orbits per day, meaning the crew or instruments aboard (if any) would experience approximately 30 sunrises and sunsets every 24 hours.