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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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 + 1 Pan, 17.7 m
Radar Cross Section
41.120 m², Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 16 hours ago
TLE from 16 hours ago
0 STARLINK-33838
1 63500U 25071H 26262.80087074 -.00015344 00000-0 -45619-3 0 9998
2 63500 53.1619 316.5715 0001976 63.3429 296.7775 15.33542898 82303Epoch: 2026-09-19T19:13Z
TLE epoch observation values (Epoch: 2026-09-19T19:13:15.231Z)
Latitude
-0.00008°
Longitude
29.55378°
Altitude
465.544 km
Speed
7.635 km/s
True Right ascension
21h 06m 17s
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
03:48:38
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
466.861 km
Perigee altitude
464.156 km
Semi-major axis
6,843.645 km
Eccentricity
0.0002
Inclination
53.1619°
RAAN
316.5715°
Arg. of periapsis
63.3429°
True anomaly
296.75728°
Mean anomaly
296.7775°
Eccentric anomaly
296.76739°
Mean motion
3.83365 °/min
Orbital period
93.91 mins
BSTAR
-0.00045619
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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. |
|---|---|---|---|---|---|---|---|
| 5 mins | 2026-09-20 12:55:43.213Z | 326.228° NNW | 2026-09-20 12:57:43.213Z | 36.622° NE | 55.221° | 2026-09-20 13:00:43.213Z | 113.662° SE |
| 5 mins | 2026-09-21 05:48:43.213Z | 206.229° SW | 2026-09-21 05:50:43.213Z | 149.304° SSE | 52.885° | 2026-09-21 05:53:43.213Z | 61.163° ENE |
| 4 mins | 2026-09-21 07:27:43.213Z | 306.242° NW | 2026-09-21 07:28:43.213Z | 331.121° NNW | 23.357° | 2026-09-21 07:31:43.213Z | 27.822° NE |
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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