STARLINK-31898, 59905
Orbit data source: Space-Track
STARLINK-31898, 59905 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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59905 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: 14 hours ago
TLE from 14 hours ago
0 STARLINK-31898
1 59905U 24100W 26306.08829948 -.00000995 00000-0 -26640-4 0 9997
2 59905 43.0014 221.2659 0000530 342.3237 17.7596 15.27581690137494Epoch: 2026-11-02T02:07Z
TLE epoch observation values (Epoch: 2026-11-02T02:07:09.075Z)
Latitude
-0.00001°
Longitude
148.10774°
Altitude
482.473 km
Speed
7.626 km/s
True Right ascension
14h 45m 03s
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
12:21:50
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
485.353 km
Perigee altitude
484.625 km
Semi-major axis
6,863.126 km
Eccentricity
0.00005
Inclination
43.0014°
RAAN
221.2659°
Arg. of periapsis
342.3237°
True anomaly
17.76145°
Mean anomaly
17.7596°
Eccentric anomaly
17.76053°
Mean motion
3.81733 °/min
Orbital period
94.31 mins
BSTAR
-0.00002664
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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-31898 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 | 2026-11-02 21:08:27.642Z | 190.21° SSW | 2026-11-02 21:10:27.642Z | 152.085° SSE | 22.213° | 2026-11-02 21:13:27.642Z | 95.274° ESE |
| 5 mins | 2026-11-02 22:47:27.642Z | 250.57° W | 2026-11-02 22:49:27.642Z | 74.822° E | 85.3° | 2026-11-02 22:52:27.642Z | 71.675° E |
| 5 mins | 2026-11-03 00:26:27.642Z | 291.754° WNW | 2026-11-03 00:28:27.642Z | 355.722° N | 50.884° | 2026-11-03 00:31:27.642Z | 72.728° E |
| 6 mins | 2026-11-03 02:05:27.642Z | 291.455° WNW | 2026-11-03 02:07:27.642Z | 328.885° NNW | 74.832° | 2026-11-03 02:11:27.642Z | 104.23° ESE |
| 5 mins | 2026-11-03 03:44:27.642Z | 258.165° W | 2026-11-03 03:46:27.642Z | 211.061° SW | 27.469° | 2026-11-03 03:49:27.642Z | 154.683° 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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