STARLINK-31206, 59028
Orbit data source: Space-Track
STARLINK-31206, 59028 is a payload satellite owned by SpaceX/Seattle (US) in LEO that was launched on Sun, 25 Feb 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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59028 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: 23 hours ago
TLE from 23 hours ago
0 STARLINK-31206
1 59028U 24038F 25348.67230881 .00003292 00000-0 12897-3 0 9994
2 59028 43.0017 82.1482 0000991 235.7840 124.2918 15.27611120102527Epoch: 2025-12-14T16:08Z
TLE epoch observation values (Epoch: 2025-12-14T16:08:07.481Z)
Latitude
0°
Longitude
116.53517°
Altitude
483.115 km
Speed
7.625 km/s
True Right ascension
05h 28m 35s
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
13:26:10
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
485.581 km
Perigee altitude
484.221 km
Semi-major axis
6,863.038 km
Eccentricity
0.0001
Inclination
43.0017°
RAAN
82.1482°
Arg. of periapsis
235.784°
True anomaly
124.30118°
Mean anomaly
124.2918°
Eccentric anomaly
124.29649°
Mean motion
3.81741 °/min
Orbital period
94.3 mins
BSTAR
0.00012897
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Other satellites on launch #38 in the year 2024 (2024-02-25 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-31206 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 | 2025-12-15 16:12:35.459Z | 251.104° W | 2025-12-15 16:14:35.459Z | 215.279° SW | 15.92° | 2025-12-15 16:16:35.459Z | 180.68° SSW |
| 4 mins | 2025-12-16 09:09:35.459Z | 195.291° SSW | 2025-12-16 09:11:35.459Z | 132.403° SE | 28.636° | 2025-12-16 09:13:35.459Z | 91.166° ESE |
| 6 mins | 2025-12-16 10:47:35.459Z | 265.411° W | 2025-12-16 10:49:35.459Z | 305.6° NW | 42.063° | 2025-12-16 10:53:35.459Z | 70.742° E |
| 6 mins | 2025-12-16 12:26:35.459Z | 291.608° WNW | 2025-12-16 12:29:35.459Z | 33.479° NE | 36.976° | 2025-12-16 12:32:35.459Z | 81.621° E |
| 6 mins | 2025-12-16 14:05:35.459Z | 284.406° WNW | 2025-12-16 14:08:35.459Z | 150.973° SSE | 42.281° | 2025-12-16 14:11:35.459Z | 117.487° 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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