GLOBALSTAR M087, 52888
Orbit data source: Space-Track
GLOBALSTAR M087, 52888 is a payload satellite owned by Globalstar (US) in LEO that was launched on Sun, 19 Jun 2022 UTC via an FALCON 9 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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52888 intel report (Beta)
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Identifier
Orbit
Country
USRelated business
Manufacturer
Thales Alenia
Mission
Operational Commercial Communications
Bus & Motor
PRISMA?, LS-400 AOCS?
Mass
715 kg wet, ~500 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Box + 2 Pan, 6.3 m
Radar Cross Section
28.800 m², Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 5 hours ago
TLE from 5 hours ago
0 GLOBALSTAR M087
1 52888U 22064A 26307.60583817 -.00000090 00000-0 78400-4 0 9994
2 52888 52.0018 358.0018 0000125 146.8683 213.2191 12.62263548208747Epoch: 2026-11-03T14:32Z
TLE epoch observation values (Epoch: 2026-11-03T14:32:24.417Z)
Latitude
-0.00008°
Longitude
97.0339°
Altitude
1,414.379 km
Speed
7.154 km/s
True Right ascension
23h 52m 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
15:07:43
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,414.105 km
Perigee altitude
1,413.91 km
Semi-major axis
7,792.145 km
Eccentricity
0.00001
Inclination
52.0018°
RAAN
358.0018°
Arg. of periapsis
146.8683°
True anomaly
213.21832°
Mean anomaly
213.2191°
Eccentric anomaly
213.21871°
Mean motion
3.15542 °/min
Orbital period
114.09 mins
BSTAR
0.0000784
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Other satellites on launch #64 in the year 2022 (2022-06-19 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 M087 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. |
|---|---|---|---|---|---|---|---|
| 9 mins | 2026-11-04 03:56:57.503Z | 154.097° SSE | 2026-11-04 04:01:57.503Z | 117.829° SE | 16.832° | 2026-11-04 04:05:57.503Z | 88.115° E |
| 15 mins | 2026-11-04 05:52:57.503Z | 215.091° SW | 2026-11-04 05:59:57.503Z | 150.542° SSE | 68.224° | 2026-11-04 06:07:57.503Z | 56.253° ENE |
| 14 mins | 2026-11-04 07:53:57.503Z | 268.449° W | 2026-11-04 08:00:57.503Z | 347.299° N | 49.384° | 2026-11-04 08:07:57.503Z | 49.318° ENE |
| 14 mins | 2026-11-04 09:55:57.503Z | 304.761° NW | 2026-11-04 10:01:57.503Z | 2.024° NNE | 37.202° | 2026-11-04 10:09:57.503Z | 68.794° E |
| 15 mins | 2026-11-04 11:55:57.503Z | 311.437° NW | 2026-11-04 12:02:57.503Z | 16.735° NNE | 58.218° | 2026-11-04 12:10:57.503Z | 105.031° ESE |
| 15 mins | 2026-11-04 13:55:57.503Z | 298.863° NW | 2026-11-04 14:02:57.503Z | 232.354° WSW | 52.36° | 2026-11-04 14:10:57.503Z | 156.349° SSE |
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 |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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