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). Payloads include a variety of satellites, spacecraft, and rockets 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)
GLOBALSTAR M002 details
| Identifier | |
| Orbit | LEO |
| Last TLE update | 13 hours ago |
| Origin | |
| 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 | Payload Rocket body Debris |
| Shape & HBR | Box + 2 Pan, 12 m |
| Radar Cross Section | 5.587 m², Large (>1 m²) |
Expand to show TLE details & history
TLE from 13 hours ago
0 GLOBALSTAR M002
1 25164U 98008C 24361.27581506 -.00000093 00000-0 -32522-3 0 9994
2 25164 52.0037 313.7505 0000917 177.6410 182.4414 11.61507097164040Epoch: 2024-12-26T06:37Z
Definitive object data (Epoch: 2024-12-26T06:37:10.421Z)
| Latitude | -0.00004° |
| Longitude | 119.19951° |
| Altitude | 1,859.344 km |
| Speed | 6.958 km/s |
| True Right ascension | 20h 55m 00s |
| True Declination | 0° 00' 00" |
| Sunlit | Object was in daylight at TLE epoch |
Visualization TLE readout
| Latitude | 21.15184° |
| Longitude | -79.6938° |
| Altitude | 1,857.647 km |
| Speed | 6.961 km/s |
| Apparent Right ascension | 07h 30m 19s |
| Apparent Declination | -5° 03' 48" |
| Sunlit | Object is in full shadow |
Visualization observer readout
| Local Sidereal Time | 19:16:01 |
| Azimuth | 353.785° N |
| Elevation | -54.999° |
| Doppler factor | 1 |
Orbital elements
| Apogee altitude | 1,859.07 km |
| Perigee altitude | 1,857.56 km |
| Semi-major axis | 8,236.452 km |
| Eccentricity | 0.0000917 |
| Inclination | 52.0037° |
| RAAN | 313.7505° |
| Arg. of periapsis | 177.641° |
| True anomaly | 182.44095° |
| Mean anomaly | 182.4414° |
| Eccentric anomaly | 182.44118° |
| Mean motion | 2.90357 °/min |
| BSTAR | -0.00032522 |
| Orbital period | 123.99 mins |
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Other satellites on launch #8 in the year 1998 (1998-02-14 UTC)
| GLOBALSTAR M001, 25162 |
| GLOBALSTAR M004, 25163 |
| GLOBALSTAR M002, 25164 |
| GLOBALSTAR M003, 25165 |
| DELTA 2 R/B, 25166 (Decayed) |
| GLOBALSTAR DEB, 25350 (Decayed) |
| GLOBALSTAR M004 DEB, 43356 |
| GLOBALSTAR M004 DEB, 43357 |
GLOBALSTAR M002 Visibility forecast
Observer location: undefined°, undefined
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. |
|---|---|---|---|---|---|---|---|
| 12 mins | 2024-12-26 21:10:17.099Z | 151.153° SSE | 2024-12-26 21:16:17.099Z | 116.122° SE | 16.762° | 2024-12-26 21:22:17.099Z | 81.122° E |
| 19 mins | 2024-12-26 23:16:17.099Z | 211.74° SW | 2024-12-26 23:25:17.099Z | 132.143° SE | 42.771° | 2024-12-26 23:35:17.099Z | 55.578° ENE |
| 19 mins | 2024-12-27 01:27:17.099Z | 263.465° W | 2024-12-27 01:36:17.099Z | 336.67° NNW | 39.622° | 2024-12-27 01:46:17.099Z | 53.664° ENE |
| 19 mins | 2024-12-27 03:40:17.099Z | 298.626° NW | 2024-12-27 03:49:17.099Z | 6.799° NNE | 35.131° | 2024-12-27 03:59:17.099Z | 76.132° E |
| 20 mins | 2024-12-27 05:52:17.099Z | 309.016° NW | 2024-12-27 06:01:17.099Z | 21.419° NNE | 43.694° | 2024-12-27 06:12:17.099Z | 117.547° SE |
| 18 mins | 2024-12-27 08:03:17.099Z | 295.822° NW | 2024-12-27 08:11:17.099Z | 239.564° WSW | 34.038° | 2024-12-27 08:21:17.099Z | 168.426° S |
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