GLOBALSTAR M002, 25164
Orbit data source: Space-Track
GLOBALSTAR M002, 25164 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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25164 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: 10 hours ago
TLE from 10 hours ago
0 GLOBALSTAR M002
1 25164U 98008C 26090.42402762 -.00000085 00000-0 -16142-3 0 9999
2 25164 52.0002 240.0008 0000565 327.4330 32.6455 11.61515599217447Epoch: 2026-03-31T10:10Z
TLE epoch observation values (Epoch: 2026-03-31T10:10:35.986Z)
Latitude
-0.00001°
Longitude
-101.45057°
Altitude
1,858.157 km
Speed
6.959 km/s
True Right ascension
16h 00m 00s
True Declination
0° 00' 00"
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
01:21:29
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,858.741 km
Perigee altitude
1,857.81 km
Semi-major axis
8,236.412 km
Eccentricity
0.00006
Inclination
52.0002°
RAAN
240.0008°
Arg. of periapsis
327.433°
True anomaly
32.64899°
Mean anomaly
32.6455°
Eccentric anomaly
32.64725°
Mean motion
2.9036 °/min
Orbital period
123.98 mins
BSTAR
-0.00016142
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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 M002 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. |
|---|---|---|---|---|---|---|---|
| 18 mins | 2026-03-31 21:09:11.112Z | 295.962° NW | 2026-03-31 21:18:11.112Z | 232.344° WSW | 32.643° | 2026-03-31 21:27:11.112Z | 171.958° S |
| 18 mins | 2026-04-01 11:03:11.112Z | 186.493° SSW | 2026-04-01 11:12:11.112Z | 120.916° SE | 32.661° | 2026-04-01 11:21:11.112Z | 62.439° ENE |
| 20 mins | 2026-04-01 13:12:11.112Z | 240.908° WSW | 2026-04-01 13:22:11.112Z | 341.062° N | 44.079° | 2026-04-01 13:32:11.112Z | 52.134° ENE |
| 19 mins | 2026-04-01 15:25:11.112Z | 285.165° WNW | 2026-04-01 15:34:11.112Z | 353.352° N | 35.331° | 2026-04-01 15:44:11.112Z | 63.192° ENE |
| 19 mins | 2026-04-01 17:38:11.112Z | 308.208° NW | 2026-04-01 17:47:11.112Z | 23.4° NE | 39.081° | 2026-04-01 17:57:11.112Z | 96.602° ESE |
Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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