STARLINK-33806, 63723
Orbit data source: Space-Track
STARLINK-33806, 63723 is a payload satellite owned by SpaceX/Seattle (US) in LEO that was launched on Mon, 28 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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63723 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: 16 hours ago
TLE from 16 hours ago
0 STARLINK-33806
1 63723U 25087AC 25348.93263929 .00014454 00000-0 49947-3 0 9992
2 63723 53.1597 253.1931 0001711 56.7088 303.4076 15.30180501 36221Epoch: 2025-12-14T22:23Z
TLE epoch observation values (Epoch: 2025-12-14T22:23:00.034Z)
Latitude
-0.00007°
Longitude
-166.39555°
Altitude
475.527 km
Speed
7.63 km/s
True Right ascension
16h 52m 46s
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
13:23:46
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
476.702 km
Perigee altitude
474.357 km
Semi-major axis
6,853.667 km
Eccentricity
0.00017
Inclination
53.1597°
RAAN
253.1931°
Arg. of periapsis
56.7088°
True anomaly
303.39123°
Mean anomaly
303.4076°
Eccentric anomaly
303.39942°
Mean motion
3.82524 °/min
Orbital period
94.11 mins
BSTAR
0.00049947
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Other satellites on launch #87 in the year 2025 (2025-04-28 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-33806 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 | 2025-12-15 20:31:11.954Z | 230.717° WSW | 2025-12-15 20:33:11.954Z | 236.508° WSW | 42.214° | 2025-12-15 20:37:11.954Z | 49.436° ENE |
| 4 mins | 2025-12-16 01:28:11.954Z | 342.154° N | 2025-12-16 01:30:11.954Z | 17.655° NNE | 16.335° | 2025-12-16 01:32:11.954Z | 55.201° ENE |
| 6 mins | 2025-12-16 03:06:11.954Z | 314.091° NW | 2025-12-16 03:09:11.954Z | 101.508° ESE | 42.126° | 2025-12-16 03:12:11.954Z | 125.991° 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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