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: 21 hours ago
TLE from 21 hours ago
0 STARLINK-33984
1 63830U 25092AC 25310.61924898 .00036736 00000-0 13368-2 0 9994
2 63830 42.9996 147.4787 0001637 264.9594 95.1071 15.27606017 29790Epoch: 2025-11-06T14:51Z
TLE epoch observation values (Epoch: 2025-11-06T14:51:43.111Z)
Latitude
-0.00002°
Longitude
-121.52592°
Altitude
482.847 km
Speed
7.626 km/s
True Right ascension
09h 49m 54s
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
07:47:52
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
486.04 km
Perigee altitude
483.793 km
Semi-major axis
6,863.053 km
Eccentricity
0.00016
Inclination
42.9996°
RAAN
147.4787°
Arg. of periapsis
264.9594°
True anomaly
95.12578°
Mean anomaly
95.1071°
Eccentric anomaly
95.11644°
Mean motion
3.81739 °/min
Orbital period
94.31 mins
BSTAR
0.0013368
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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 | 2025-11-07 16:09:37.576Z | 211.162° SW | 2025-11-07 16:12:37.576Z | 156.213° SSE | 27.153° | 2025-11-07 16:15:37.576Z | 89.968° E |
| 5 mins | 2025-11-07 17:49:37.576Z | 263.491° W | 2025-11-07 17:51:37.576Z | 347.239° N | 43.91° | 2025-11-07 17:54:37.576Z | 69.705° E |
| 5 mins | 2025-11-07 19:28:37.576Z | 293.741° NW | 2025-11-07 19:30:37.576Z | 351.515° N | 38.051° | 2025-11-07 19:33:37.576Z | 76.962° E |
| 5 mins | 2025-11-07 21:07:37.576Z | 285.376° WNW | 2025-11-07 21:09:37.576Z | 254.653° W | 43.799° | 2025-11-07 21:12:37.576Z | 114.92° 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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