GLOBALSTAR M001, 25162
Orbit data source: Space-Track
GLOBALSTAR M001, 25162 is a payload satellite owned by Globalstar (US) in LEO that was launched on Sat, 14 Feb 1998 UTC via a DELTA 7420-10C launch vehicle from the Air Force Eastern Test Range (AFETR). Payload-class satellites include a variety of spacecraft equipped with specific instruments for various scientific and technological missions. These include communications satellites like Starlink; space stations such as the ISS; scientific satellites like the Hubble; Earth observation satellites from companies like Planet Labs, Umbra, and HawkEye 360; GPS; miniature CubeSats for education and research; and military/defense satellites.
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25162 intel report (Beta)
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Identifier
Orbit
Country
US / GLOBRelated business
Manufacturer
SS/Loral
Mission
Non-operational Commercial Communications
Bus & Motor
LS-400, Unknown motor
Mass
450 kg wet, 380 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Box + 2 Pan, 6.0 m
Radar Cross Section
5.587 m², Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 14 hours ago
TLE from 14 hours ago
0 GLOBALSTAR M001
1 25162U 98008A 26140.55934566 -.00000100 00000-0 -23134-4 0 9997
2 25162 52.0037 71.2514 0000985 266.0387 265.3996 12.38231951285504Epoch: 2026-05-20T13:25Z
TLE epoch observation values (Epoch: 2026-05-20T13:25:27.465Z)
Latitude
6.71528°
Longitude
166.41817°
Altitude
1,514.226 km
Speed
7.109 km/s
True Right ascension
16h 23m 59s
True Declination
6° 40' 45"
Sunlit
Visualization orbit readout
Latitude
Unknown
Longitude
Unknown
Altitude
Unknown
Speed
Unknown
Apparent Right ascension
Unknown
Apparent Declination
Unknown
Sunlit
Visualization observer readout
Local Sidereal Time
12:42:44
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,515.271 km
Perigee altitude
1,513.716 km
Semi-major axis
7,892.631 km
Eccentricity
0.0001
Inclination
52.0037°
RAAN
71.2514°
Arg. of periapsis
266.0387°
True anomaly
265.38835°
Mean anomaly
265.3996°
Eccentric anomaly
265.39397°
Mean motion
3.09536 °/min
Orbital period
116.3 mins
BSTAR
-0.000023134
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Other satellites on launch #8 in the year 1998 (1998-02-14 UTC)
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You can import UDL-sourced sensor .json files into the Sandbox to generate a visibility chart that accounts for multi-vendor sensor geometry.GLOBALSTAR M001 Visibility forecast
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Span | Click to sort rows by Start time (UTC) header in descending order | Start Az. | Max El. time (UTC) | Max El. Az. | Max El. | End time (UTC) | End Az. |
|---|---|---|---|---|---|---|---|
| 17 mins | 2026-05-21 04:30:58.647Z | 308.577° NW | 2026-05-21 04:39:58.647Z | 64.403° ENE | 44.236° | 2026-05-21 04:47:58.647Z | 121.88° SE |
| 14 mins | 2026-05-21 06:34:58.647Z | 288.055° WNW | 2026-05-21 06:40:58.647Z | 236.542° WSW | 29.512° | 2026-05-21 06:48:58.647Z | 174.302° S |
| 9 mins | 2026-05-21 19:36:58.647Z | 150.43° SSE | 2026-05-21 19:40:58.647Z | 122.07° SE | 16.961° | 2026-05-21 19:45:58.647Z | 86.076° E |
| 16 mins | 2026-05-21 21:34:58.647Z | 215.033° SW | 2026-05-21 21:41:58.647Z | 148.146° SSE | 43.18° | 2026-05-21 21:50:58.647Z | 55.381° ENE |
| 15 mins | 2026-05-21 23:37:58.647Z | 268.479° W | 2026-05-21 23:44:58.647Z | 339.229° N | 37.771° | 2026-05-21 23:52:58.647Z | 50.821° ENE |
| 15 mins | 2026-05-22 01:41:58.647Z | 302.093° NW | 2026-05-22 01:48:58.647Z | 3.936° NNE | 32.326° | 2026-05-22 01:56:58.647Z | 69.976° E |
Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
Click to sort rows by RSO header in ascending order | Click to sort rows by Country header in ascending order | Click to sort rows by Type header in ascending order | Click to sort rows by Inclination Δ header in ascending order | Click to sort rows by RAAN Δ header in ascending order | Click to sort rows by Coplanar Angle header in ascending order | Click to sort rows by SMA Δ header in ascending order | Click to sort rows by Orbital period header in ascending order | Click to sort rows by <5km Md TCA header in descending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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