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: 9 hours ago
TLE from 9 hours ago
0 GLOBALSTAR M087
1 52888U 22064A 26305.86378441 -.00000092 00000-0 68057-4 0 9994
2 52888 52.0020 3.3052 0000177 148.4739 211.6138 12.62263503208525Epoch: 2026-11-01T20:43Z
TLE epoch observation values (Epoch: 2026-11-01T20:43:50.973Z)
Latitude
-0.00003°
Longitude
11.19375°
Altitude
1,414.415 km
Speed
7.154 km/s
True Right ascension
00h 13m 13s
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
01:34:33
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,414.146 km
Perigee altitude
1,413.87 km
Semi-major axis
7,792.145 km
Eccentricity
0.00002
Inclination
52.002°
RAAN
3.3052°
Arg. of periapsis
148.4739°
True anomaly
211.61274°
Mean anomaly
211.6138°
Eccentric anomaly
211.61327°
Mean motion
3.15542 °/min
Orbital period
114.09 mins
BSTAR
0.000068057
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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. |
|---|---|---|---|---|---|---|---|
| 16 mins | 2026-11-02 06:21:56.690Z | 214.235° SW | 2026-11-02 06:29:56.690Z | 120.222° SE | 66.469° | 2026-11-02 06:37:56.690Z | 55.778° ENE |
| 15 mins | 2026-11-02 08:22:56.690Z | 266.696° W | 2026-11-02 08:29:56.690Z | 342.282° N | 50.437° | 2026-11-02 08:37:56.690Z | 51.225° ENE |
| 14 mins | 2026-11-02 10:24:56.690Z | 303.243° NW | 2026-11-02 10:30:56.690Z | 358.472° N | 37.061° | 2026-11-02 10:38:56.690Z | 67.448° ENE |
| 15 mins | 2026-11-02 12:25:56.690Z | 313.44° NW | 2026-11-02 12:32:56.690Z | 37.156° NE | 57.367° | 2026-11-02 12:40:56.690Z | 105.604° ESE |
| 14 mins | 2026-11-02 14:25:56.690Z | 297.381° NW | 2026-11-02 14:31:56.690Z | 238.507° WSW | 53.407° | 2026-11-02 14:39:56.690Z | 155.791° SSE |
| 14 mins | 2026-11-03 05:08:56.690Z | 185.015° SSW | 2026-11-03 05:15:56.690Z | 120.639° SE | 35.971° | 2026-11-03 05:22:56.690Z | 65.242° 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 |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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