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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). 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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Identifier
25622, 1999-004B
Orbit
LEO
Country
Flag of UnknownUnknown / GLOB
Related business
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)
1999-02-09 (27 years ago)
Launch vehicle
SOYUZ-U-PVB
Launch site
Tyuratam Missile And Space Complex (TTMTR)
Object type
Payload
Rocket body
Debris
Shape & HBR
Box + 2 Pan, 6.0 m
Radar Cross Section
5.587 m², Large (>1 m²)

Expand to show TLE details & history
Last TLE update: 20 hours ago

TLE from 20 hours ago
0 GLOBALSTAR M040
1 25622U 99004B   26032.55813452 -.00000069  00000-0  19183-3 0  9996
2 25622  51.9919  79.4855 0001329 157.4862   6.8059 12.62028187244217
Epoch: 2026-02-01T13:23Z
TLE epoch observation values (Epoch: 2026-02-01T13:23:42.822Z)
Latitude
12.31483°
Longitude
-82.98323°
Altitude
1,413.489 km
Speed
7.156 km/s
True Right ascension
16h 38m 50s
True Declination
12° 14' 58"
Sunlit
Object was in daylight at epoch
Visualization orbit readout
Latitude
Unknown
Longitude
Unknown
Altitude
Unknown
Speed
Unknown
Apparent Right ascension
Unknown
Apparent Declination
Unknown
Sunlit
N/A
Visualization observer readout
Local Sidereal Time
10:45:59
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,416.013 km
Perigee altitude
1,413.942 km
Semi-major axis
7,793.115 km
Eccentricity
0.00013
Inclination
51.9919°
RAAN
79.4855°
Arg. of periapsis
157.4862°
True anomaly
6.80771°
Mean anomaly
6.8059°
Eccentric anomaly
6.8068°
Mean motion
3.15483 °/min
Orbital period
114.11 mins
BSTAR
0.00019183
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Other satellites on launch #4 in the year 1999 (1999-02-09 UTC)

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