GLOBALSTAR M040, 25622
Orbit data source: Space-Track
GLOBALSTAR M040, 25622 is a payload satellite owned by Globalstar (US) in LEO that was launched on Tue, 09 Feb 1999 UTC via a SOYUZ-U-PVB launch vehicle from the Tyuratam Missile And Space Complex (TTMTR). 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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25622 intel report (Beta)
GLOBALSTAR M040 details
| Identifier | |
| Orbit | LEO |
| Last TLE update | 20 hours ago |
| Origin | |
| Manufacturer | SS/Loral |
| Mission | Non-operational Commercial Communications |
| Bus & Motor | LS-400, LS-400 AOCS |
| 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 20 hours ago
0 GLOBALSTAR M040
1 25622U 99004B 24360.63832719 -.00000042 00000-0 34399-3 0 9991
2 25622 51.9896 225.7956 0001663 49.3583 340.0139 12.61995588193345Epoch: 2024-12-25T15:19Z
Definitive object data (Epoch: 2024-12-25T15:19:11.469Z)
| Latitude | 22.78194° |
| Longitude | -79.56678° |
| Altitude | 1,414.067 km |
| Speed | 7.157 km/s |
| True Right ascension | 16h 19m 26s |
| True Declination | 22° 40' 11" |
| Sunlit | Object was in daylight at TLE epoch |
Visualization TLE readout
| Latitude | -14.34377° |
| Longitude | 90.31569° |
| Altitude | 1,419.46 km |
| Speed | 7.151 km/s |
| Apparent Right ascension | 01h 44m 39s |
| Apparent Declination | -31° 04' 46" |
| Sunlit | Object is in full shadow |
Visualization observer readout
| Local Sidereal Time | 10:34:27 |
| Azimuth | 267.734° W |
| Elevation | -50.771° |
| Doppler factor | 1 |
Orbital elements
| Apogee altitude | 1,416.408 km |
| Perigee altitude | 1,413.816 km |
| Semi-major axis | 7,793.249 km |
| Eccentricity | 0.0001663 |
| Inclination | 51.9896° |
| RAAN | 225.7956° |
| Arg. of periapsis | 49.3583° |
| True anomaly | 340.00739° |
| Mean anomaly | 340.0139° |
| Eccentric anomaly | 340.01064° |
| Mean motion | 3.15475 °/min |
| BSTAR | 0.00034399 |
| Orbital period | 114.11 mins |
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Other satellites on launch #4 in the year 1999 (1999-02-09 UTC)
| GLOBALSTAR M023, 25621 |
| GLOBALSTAR M040, 25622 |
| GLOBALSTAR M036, 25623 |
| GLOBALSTAR M038, 25624 |
| SL-4 R/B(1), 25625 (Decayed) |
GLOBALSTAR M040 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 15:59:09.109Z | 166.872° S | 2024-12-26 16:05:09.109Z | 117.564° SE | 22.268° | 2024-12-26 16:11:09.109Z | 73.096° E |
| 16 mins | 2024-12-26 17:56:09.109Z | 227.104° WSW | 2024-12-26 18:03:09.109Z | 195.833° SSW | 44.758° | 2024-12-26 18:12:09.109Z | 53.172° ENE |
| 15 mins | 2024-12-26 19:57:09.109Z | 276° WNW | 2024-12-26 20:04:09.109Z | 343.912° N | 34.806° | 2024-12-26 20:12:09.109Z | 53.216° ENE |
| 14 mins | 2024-12-26 21:59:09.109Z | 306.786° NW | 2024-12-26 22:06:09.109Z | 14.458° NNE | 31.991° | 2024-12-26 22:13:09.109Z | 73.789° E |
| 15 mins | 2024-12-27 00:00:09.109Z | 311.499° NW | 2024-12-27 00:07:09.109Z | 47.387° ENE | 43.269° | 2024-12-27 00:15:09.109Z | 116.725° SE |
| 13 mins | 2024-12-27 02:00:09.109Z | 290.661° WNW | 2024-12-27 02:06:09.109Z | 233.725° WSW | 32.202° | 2024-12-27 02:13:09.109Z | 170.665° S |
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