STARLINK-33984, 63830
Orbit data source: Space-Track
STARLINK-33984, 63830 is a payload satellite owned by SpaceX/Seattle (US) in LEO that was launched on Sun, 04 May 2025 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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63830 intel report (Beta)
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Edit Public Description
Identifier
Orbit
Country
USRelated business
Manufacturer
SpaceX/Seattle
Mission
Operational spacecraft
Bus & Motor
STARLINK V2MO, Unknown motor
Mass
575 kg wet, ~530 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Unknown shape, 17.7 m
Radar Cross Section
Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 2 days ago
TLE from 2 days ago
0 STARLINK-33984
1 63830U 25092AC 25305.91142224 .00031722 00000-0 11560-2 0 9998
2 63830 42.9999 174.0670 0001142 273.6431 86.4290 15.27617419 29073Epoch: 2025-11-01T21:52Z
TLE epoch observation values (Epoch: 2025-11-01T21:52:26.881Z)
Latitude
-0.00002°
Longitude
164.52026°
Altitude
482.664 km
Speed
7.626 km/s
True Right ascension
11h 36m 16s
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
00:05:57
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
485.666 km
Perigee altitude
484.099 km
Semi-major axis
6,863.019 km
Eccentricity
0.00011
Inclination
42.9999°
RAAN
174.067°
Arg. of periapsis
273.6431°
True anomaly
86.44206°
Mean anomaly
86.429°
Eccentric anomaly
86.43553°
Mean motion
3.81742 °/min
Orbital period
94.3 mins
BSTAR
0.001156
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Other satellites on launch #92 in the year 2025 (2025-05-04 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-33984 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. |
|---|---|---|---|---|---|---|---|
| 6 mins | 2025-11-04 17:32:46.459Z | 211.604° SW | 2025-11-04 17:35:46.459Z | 147.609° SSE | 28.809° | 2025-11-04 17:38:46.459Z | 86.593° E |
| 5 mins | 2025-11-04 19:12:46.459Z | 267.575° W | 2025-11-04 19:14:46.459Z | 21.227° NNE | 42.731° | 2025-11-04 19:17:46.459Z | 69.995° E |
| 5 mins | 2025-11-04 20:51:46.459Z | 296.806° NW | 2025-11-04 20:53:46.459Z | 9.367° NNE | 38.391° | 2025-11-04 20:56:46.459Z | 79.432° E |
| 5 mins | 2025-11-04 22:30:46.459Z | 283.11° WNW | 2025-11-04 22:32:46.459Z | 198.721° SSW | 44.118° | 2025-11-04 22:35:46.459Z | 116.999° SE |
| 4 mins | 2025-11-05 00:09:46.459Z | 245.787° WSW | 2025-11-05 00:11:46.459Z | 206.558° SW | 16.529° | 2025-11-05 00:13:46.459Z | 174.146° S |
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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