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GPM

NORAD 39574 Payload LEO 2014-009C ● Active
CONNECTING… LEO · NORAD 39574
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Altitude (km)
Speed (km/s)
Latitude
Longitude
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🛰️ Orbital Parameters
Perigee
425 km
Apogee
441 km
Inclination
65.0°
Period
93.2 min
Mean Motion
15.44609240 rev/day
TLE Epoch
2026-06-19 05:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude433 km
Orbital Velocity27,554 km/h
Velocity7.65 km/s
Orbital Period93 minutes
Orbits / Day15.45
Eccentricity0.0012
Semi-Major Axis6,804 km
Est. Orbital Lifetime~1–3 years
🚀 Launch & Identity
Country / Operator
🇯🇵 National Aeronautics and Space Administration (NASA)/JAXA (Japan)
Launch Date
2014-02-27
Launch Site
TNSTA
Int'l Designator
2014-009C
Object Type
Payload
RCS Size
Large (>1 m²)
📖 About This Object
GPM is an active satellite operated by National Aeronautics and Space Administration (NASA)/JAXA (Japan), launched on 2014-02-27 from TNSTA. After 12 years in orbit, it continues to be tracked by global surveillance networks. It orbits in Low Earth Orbit (LEO) at altitudes between 425 km and 441 km with an inclination of 65.0°. It travels at approximately 27,554 km/h (7.65 km/s), completing one full orbit every 93 minutes — that’s roughly 15.45 orbits per day. At its current altitude, the estimated orbital lifetime before atmospheric re-entry is ~1–3 years. Orbital Radar tracks GPM in real time using the latest two-line element set (TLE) data, providing live position, altitude, speed and orbital path updated continuously.
🌍 Orbit Context
GPM orbits at an average altitude of 433 km in the core of Low Earth Orbit, the most heavily utilised altitude band. The balance of moderate drag (limiting debris accumulation) and short signal path (enabling low-latency links and high-resolution imaging) makes this regime the default for most commercial and government missions. Within ±50 km of GPM’s average altitude, there are currently 7,374 active payloads and 143 tracked debris or rocket body fragments — notable neighbours include STARLINK-1008, STARLINK-1012, STARLINK-1017. This makes it one of the more crowded altitude bands, containing roughly 42.4% of all active satellites. With an inclination of 65.0°, GPM passes over latitudes between 65.0°N and 65.0°S, covering most populated land masses in both hemispheres. This mid-inclination band balances global coverage with efficient launch energy requirements. Japan operates approximately 189 active satellites in total, of which 9 share a similar altitude band with GPM.
❓ Frequently Asked Questions
GPM orbits in Low Earth Orbit (LEO) at altitudes between 425 km (perigee) and 441 km (apogee), with an average altitude of approximately 433 km. It completes one orbit every 93 minutes, travelling at approximately 27,554 km/h (17,121 mph).
GPM is operated by National Aeronautics and Space Administration (NASA)/JAXA (Japan). It is catalogued by the U.S. Space Surveillance Network under NORAD ID 39574. You can track GPM in real time on Orbital Radar’s live tracker or browse all operators in the operator directory.
GPM was launched on 2014-02-27 from TNSTA. At its current altitude, the estimated remaining orbital lifetime is: ~1–3 years. View the full satellite launch log.
Yes — Orbital Radar tracks GPM (NORAD ID 39574) 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.
GPM travels at approximately 27,554 km/h (17,121 mph) — roughly 7.65 km/s. It completes 15.45 orbits per day, meaning the crew or instruments aboard (if any) would experience approximately 31 sunrises and sunsets every 24 hours.