STARLINK-31969, 59889
Orbit data source: Space-Track
STARLINK-31969, 59889 is a payload satellite owned by SpaceX/Seattle (US) in LEO that was launched on Tue, 28 May 2024 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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59889 intel report (Beta)
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Edit Public Description
Identifier
Orbit
Country
USRelated business
Manufacturer
SpaceX/Seattle
Mission
Operational Commercial Communications
Bus & Motor
STARLINK V2M, Unknown motor
Mass
730 kg wet, ~700 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Box + 2 Pan, 17.7 m
Radar Cross Section
33.884 m², Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 11 hours ago
TLE from 11 hours ago
0 STARLINK-31969
1 59889U 24100E 26036.16922016 -.00000631 00000-0 -13417-4 0 9992
2 59889 42.9999 305.5713 0000471 329.4494 30.6330 15.27577237 96224Epoch: 2026-02-05T04:03Z
TLE epoch observation values (Epoch: 2026-02-05T04:03:40.621Z)
Latitude
-0.00004°
Longitude
109.32669°
Altitude
482.555 km
Speed
7.626 km/s
True Right ascension
20h 22m 17s
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
17:14:42
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
485.326 km
Perigee altitude
484.679 km
Semi-major axis
6,863.14 km
Eccentricity
0.00005
Inclination
42.9999°
RAAN
305.5713°
Arg. of periapsis
329.4494°
True anomaly
30.63575°
Mean anomaly
30.633°
Eccentric anomaly
30.63438°
Mean motion
3.81732 °/min
Orbital period
94.31 mins
BSTAR
-0.000013417
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Other satellites on launch #100 in the year 2024 (2024-05-28 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.STARLINK-31969 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. |
|---|---|---|---|---|---|---|---|
| 5 mins | 2026-02-05 21:34:03.184Z | 221.316° SW | 2026-02-05 21:36:03.184Z | 136.815° SSE | 38.882° | 2026-02-05 21:39:03.184Z | 78.191° E |
| 5 mins | 2026-02-05 23:13:03.184Z | 283.582° WNW | 2026-02-05 23:15:03.184Z | 12.447° NNE | 39.44° | 2026-02-05 23:18:03.184Z | 70.413° E |
| 5 mins | 2026-02-06 00:52:03.184Z | 297.226° NW | 2026-02-06 00:54:03.184Z | 13.915° NNE | 40.954° | 2026-02-06 00:57:03.184Z | 88.994° E |
| 5 mins | 2026-02-06 02:31:03.184Z | 269.318° W | 2026-02-06 02:33:03.184Z | 200.328° SSW | 36.382° | 2026-02-06 02:36:03.184Z | 134.497° SE |
Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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