STARLINK-33903, 63828
Orbit data source: Space-Track
STARLINK-33903, 63828 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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63828 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: 6 hours ago
TLE from 6 hours ago
0 STARLINK-33903
1 63828U 25092AA 26038.58335648 .00006175 00000-0 23357-3 0 9998
2 63828 43.0032 342.5600 0001414 286.6450 313.1274 15.27601091 5808Epoch: 2026-02-07T14:00Z
TLE epoch observation values (Epoch: 2026-02-07T14:00:01.999Z)
Latitude
-36.27648°
Longitude
-133.65155°
Altitude
492.841 km
Speed
7.619 km/s
True Right ascension
14h 16m 14s
True Declination
-36° 06' 23"
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
22:39:13
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
485.901 km
Perigee altitude
483.96 km
Semi-major axis
6,863.068 km
Eccentricity
0.00014
Inclination
43.0032°
RAAN
342.56°
Arg. of periapsis
286.645°
True anomaly
313.11557°
Mean anomaly
313.1274°
Eccentric anomaly
313.12149°
Mean motion
3.81738 °/min
Orbital period
94.31 mins
BSTAR
0.00023357
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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-33903 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 | 2026-02-08 00:10:49.286Z | 234.422° WSW | 2026-02-08 00:13:49.286Z | 114.139° SE | 39.9° | 2026-02-08 00:16:49.286Z | 75.557° E |
| 6 mins | 2026-02-08 01:49:49.286Z | 280.172° WNW | 2026-02-08 01:52:49.286Z | 24.189° NE | 37.6° | 2026-02-08 01:55:49.286Z | 71.975° E |
| 5 mins | 2026-02-08 03:29:49.286Z | 297.995° NW | 2026-02-08 03:31:49.286Z | 36.59° NE | 41.554° | 2026-02-08 03:34:49.286Z | 93.418° ESE |
| 5 mins | 2026-02-08 05:08:49.286Z | 261.413° W | 2026-02-08 05:10:49.286Z | 192.029° SSW | 32.335° | 2026-02-08 05:13:49.286Z | 138.824° SSE |
Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
Click to sort rows by RSO header in ascending order | Click to sort rows by Country header in ascending order | Click to sort rows by Type header in ascending order | Click to sort rows by Inclination Δ header in ascending order | Click to sort rows by RAAN Δ header in ascending order | Click to sort rows by Coplanar Angle header in ascending order | Click to sort rows by SMA Δ header in ascending order | Click to sort rows by Orbital period header in ascending order | Click to sort rows by <5km Md TCA header in descending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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