STARLINK-33838, 63500
Orbit data source: Space-Track
STARLINK-33838, 63500 is a payload satellite owned by SpaceX/Seattle (US) in LEO that was launched on Mon, 07 Apr 2025 UTC via an FALCON 9 launch vehicle from the Air Force Western Test Range (AFWTR). 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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63500 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 V2MO, Unknown motor
Mass
575 kg wet, ~530 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Box + 2 Pan, 17.7 m
Radar Cross Section
36.964 m², Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 12 hours ago
TLE from 12 hours ago
0 STARLINK-33838
1 63500U 25071H 26002.60550420 .00037527 00000-0 12733-2 0 9993
2 63500 53.1597 86.7698 0001585 98.1475 261.9706 15.30186314 42440Epoch: 2026-01-02T14:31Z
TLE epoch observation values (Epoch: 2026-01-02T14:31:55.562Z)
Latitude
-0.00001°
Longitude
126.54497°
Altitude
476.308 km
Speed
7.629 km/s
True Right ascension
05h 47m 04s
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
01:58:55
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
476.599 km
Perigee altitude
474.426 km
Semi-major axis
6,853.649 km
Eccentricity
0.00016
Inclination
53.1597°
RAAN
86.7698°
Arg. of periapsis
98.1475°
True anomaly
261.95262°
Mean anomaly
261.9706°
Eccentric anomaly
261.96161°
Mean motion
3.82525 °/min
Orbital period
94.11 mins
BSTAR
0.0012733
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Other satellites on launch #71 in the year 2025 (2025-04-07 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-33838 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 | 2026-01-03 07:56:31.116Z | 216.122° SW | 2026-01-03 07:59:31.116Z | 157.074° SSE | 40.854° | 2026-01-03 08:02:31.116Z | 58.698° ENE |
| 4 mins | 2026-01-03 09:36:31.116Z | 302.662° NW | 2026-01-03 09:37:31.116Z | 324.784° NNW | 20.36° | 2026-01-03 09:40:31.116Z | 24.351° NE |
| 5 mins | 2026-01-03 14:32:31.116Z | 325.81° NNW | 2026-01-03 14:34:31.116Z | 21.031° NNE | 37.897° | 2026-01-03 14:37:31.116Z | 110.167° ESE |
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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