STARLINK-31676, 59900
Orbit data source: Space-Track
STARLINK-31676, 59900 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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59900 intel report (Beta)
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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: 8 hours ago
TLE from 8 hours ago
0 STARLINK-31676
1 59900U 24100R 26306.33335647 .00013342 00000-0 49358-3 0 9996
2 59900 43.0015 223.3973 0001446 273.3787 330.2657 15.27574640 5821Epoch: 2026-11-02T08:00Z
TLE epoch observation values (Epoch: 2026-11-02T08:00:01.999Z)
Latitude
-37.83949°
Longitude
-62.29232°
Altitude
493.361 km
Speed
7.619 km/s
True Right ascension
06h 37m 18s
True Declination
-37° 39' 60"
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
12:16:39
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
486.002 km
Perigee altitude
484.018 km
Semi-major axis
6,863.147 km
Eccentricity
0.00014
Inclination
43.0015°
RAAN
223.3973°
Arg. of periapsis
273.3787°
True anomaly
330.25748°
Mean anomaly
330.2657°
Eccentric anomaly
330.26159°
Mean motion
3.81732 °/min
Orbital period
94.31 mins
BSTAR
0.00049358
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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-31676 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. |
|---|---|---|---|---|---|---|---|
| 4 mins | 2026-11-02 21:15:17.690Z | 180.545° SSW | 2026-11-02 21:17:17.690Z | 140.481° SSE | 19.935° | 2026-11-02 21:19:17.690Z | 103.389° ESE |
| 6 mins | 2026-11-02 22:53:17.690Z | 246.27° WSW | 2026-11-02 22:55:17.690Z | 232.247° WSW | 68.101° | 2026-11-02 22:59:17.690Z | 72.481° E |
| 6 mins | 2026-11-03 00:32:17.690Z | 285.836° WNW | 2026-11-03 00:35:17.690Z | 25.223° NE | 47.784° | 2026-11-03 00:38:17.690Z | 74.021° E |
| 6 mins | 2026-11-03 02:11:17.690Z | 291.255° WNW | 2026-11-03 02:14:17.690Z | 56.324° ENE | 69.856° | 2026-11-03 02:17:17.690Z | 100.557° ESE |
| 4 mins | 2026-11-03 03:51:17.690Z | 252.781° W | 2026-11-03 03:52:17.690Z | 227.858° WSW | 29.586° | 2026-11-03 03:55:17.690Z | 155.955° SSE |
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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