STARLINK-32669, 62213
Orbit data source: Space-Track
STARLINK-32669, 62213 is a payload satellite owned by SpaceX/Seattle (US) in LEO that was launched on Wed, 04 Dec 2024 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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62213 intel report (Beta)
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Identifier
Orbit
Country
USRelated business
Manufacturer
SpaceX/Seattle
Mission
Operational Commercial Communications
Bus & Motor
STARLINK V2M, Unknown motor
Mass
730 kg wet, ~700 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Box + 2 Pan, 17.7 m
Radar Cross Section
33.884 m², Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 11 hours ago
TLE from 11 hours ago
0 STARLINK-32669
1 62213U 24229X 26171.38389625 .00007196 00000-0 27073-3 0 9999
2 62213 43.0047 51.0436 0001146 256.2639 103.8085 15.27582755 86262Epoch: 2026-06-20T09:12Z
TLE epoch observation values (Epoch: 2026-06-20T09:12:48.636Z)
Latitude
-0.00005°
Longitude
4.2416°
Altitude
483.005 km
Speed
7.626 km/s
True Right ascension
03h 24m 10s
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
07:17:37
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
485.772 km
Perigee altitude
484.199 km
Semi-major axis
6,863.122 km
Eccentricity
0.00011
Inclination
43.0047°
RAAN
51.0436°
Arg. of periapsis
256.2639°
True anomaly
103.82125°
Mean anomaly
103.8085°
Eccentric anomaly
103.81488°
Mean motion
3.81734 °/min
Orbital period
94.31 mins
BSTAR
0.00027073
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Other satellites on launch #229 in the year 2024 (2024-12-04 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-32669 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 | 2026-06-20 20:26:52.444Z | 250.104° W | 2026-06-20 20:29:52.444Z | 244.688° WSW | 44.366° | 2026-06-20 20:32:52.444Z | 72.071° E |
| 6 mins | 2026-06-20 22:06:52.444Z | 288.33° WNW | 2026-06-20 22:08:52.444Z | 335.817° NNW | 37.052° | 2026-06-20 22:12:52.444Z | 76.273° E |
| 6 mins | 2026-06-20 23:45:52.444Z | 290.238° WNW | 2026-06-20 23:48:52.444Z | 85.737° E | 42.316° | 2026-06-20 23:51:52.444Z | 104.32° ESE |
| 4 mins | 2026-06-21 01:25:52.444Z | 245.541° WSW | 2026-06-21 01:26:52.444Z | 220.05° SW | 24.223° | 2026-06-21 01:29:52.444Z | 157.792° S |
| 4 mins | 2026-06-21 18:21:52.444Z | 183.444° SSW | 2026-06-21 18:23:52.444Z | 141.608° SSE | 20.111° | 2026-06-21 18:25:52.444Z | 102.746° ESE |
| 6 mins | 2026-06-21 19:59:52.444Z | 249.143° W | 2026-06-21 20:01:52.444Z | 244.23° WSW | 42.491° | 2026-06-21 20:05:52.444Z | 72.247° E |
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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