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.
Focus sentinelFocus sentinel
Request partner network tasking
Focus sentinelFocus sentinel
Embed this page
Focus sentinelFocus sentinel
25622 intel report (Beta)
Focus sentinelFocus sentinel
Edit Public Description
Focus sentinelFocus sentinel
Edit Sat Name
Focus sentinelFocus sentinel
Create New Watchlist
Identifier
Orbit
Country
US / GLOBRelated 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)
Launch vehicle
Launch site
Object type
Shape & HBR
Box + 2 Pan, 6.3 m
Radar Cross Section
5.587 m², Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 21 hours ago
TLE from 21 hours ago
0 GLOBALSTAR M040
1 25622U 99004B 26302.54368727 -.00000080 00000-0 13164-3 0 9991
2 25622 51.9934 337.7385 0000986 60.6611 92.5909 12.62039752278300Epoch: 2026-10-29T13:02Z
TLE epoch observation values (Epoch: 2026-10-29T13:02:54.580Z)
Latitude
20.80555°
Longitude
-93.05144°
Altitude
1,414.937 km
Speed
7.156 km/s
True Right ascension
09h 22m 12s
True Declination
20° 42' 04"
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
05:25:40
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,415.698 km
Perigee altitude
1,414.161 km
Semi-major axis
7,793.067 km
Eccentricity
0.0001
Inclination
51.9934°
RAAN
337.7385°
Arg. of periapsis
60.6611°
True anomaly
92.60219°
Mean anomaly
92.5909°
Eccentric anomaly
92.59654°
Mean motion
3.15486 °/min
Orbital period
114.11 mins
BSTAR
0.00013164
Loading maneuver chart data...
Computing Atmospheric mass density...
Loading historical data...
Loading historical data...
Loading historical data...
Loading historical data...
Loading historical data...
Loading historical data...
Loading historical data...
Other satellites on launch #4 in the year 1999 (1999-02-09 UTC)
Did you know?
You can import UDL-sourced sensor .json files into the Sandbox to generate a visibility chart that accounts for multi-vendor sensor geometry.GLOBALSTAR M040 Visibility forecast
Loading observer location...
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 | 2026-10-30 11:33:13.506Z | 308.624° NW | 2026-10-30 11:41:13.506Z | 2.673° NNE | 75.354° | 2026-10-30 11:50:13.506Z | 121.944° SE |
| 13 mins | 2026-10-30 13:35:13.506Z | 286.793° WNW | 2026-10-30 13:41:13.506Z | 230.245° WSW | 33.706° | 2026-10-30 13:48:13.506Z | 174.601° S |
| 4 mins | 2026-10-31 02:24:13.506Z | 128.989° SE | 2026-10-31 02:26:13.506Z | 114.761° SE | 12.175° | 2026-10-31 02:28:13.506Z | 100.713° ESE |
| 15 mins | 2026-10-31 04:17:13.506Z | 205.707° SW | 2026-10-31 04:24:13.506Z | 133.239° SE | 57.299° | 2026-10-31 04:32:13.506Z | 58.242° ENE |
| 15 mins | 2026-10-31 06:17:13.506Z | 259.949° W | 2026-10-31 06:24:13.506Z | 335.443° NNW | 55.625° | 2026-10-31 06:32:13.506Z | 50.16° ENE |
| 14 mins | 2026-10-31 08:19:13.506Z | 299.35° NW | 2026-10-31 08:25:13.506Z | 353.72° N | 36.937° | 2026-10-31 08:33:13.506Z | 63.542° ENE |
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 |
|---|
CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
Authenticating...
Click to sort rows by Secondary header in ascending order | Click to sort rows by Secondary name header in ascending order | Click to sort rows by Country header in ascending order | Click to sort rows by Owner header in ascending order | Click to sort rows by Obj. Type header in ascending order | Click to sort rows by Miss dist. header in ascending order | Click to sort rows by Rel. speed header in ascending order | Click to sort rows by Apr. angle header in ascending order | Click to sort rows by TCA header in descending order |
|---|