STARLINK-32567, 61930
Orbit data source: Space-Track
STARLINK-32567, 61930 is a payload satellite owned by SpaceX/Seattle (US) in LEO that was launched on Mon, 11 Nov 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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61930 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: 1 day ago
TLE from 1 day ago
0 STARLINK-32567
1 61930U 24207U 26072.56486041 .00017094 00000-0 62895-3 0 9999
2 61930 43.0029 256.4751 0001677 272.6921 87.3738 15.27596003 75948Epoch: 2026-03-13T13:33Z
TLE epoch observation values (Epoch: 2026-03-13T13:33:23.939Z)
Latitude
-0.00007°
Longitude
-118.07329°
Altitude
482.724 km
Speed
7.626 km/s
True Right ascension
17h 05m 54s
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
20:50:45
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
486.097 km
Perigee altitude
483.795 km
Semi-major axis
6,863.083 km
Eccentricity
0.00017
Inclination
43.0029°
RAAN
256.4751°
Arg. of periapsis
272.6921°
True anomaly
87.393°
Mean anomaly
87.3738°
Eccentric anomaly
87.3834°
Mean motion
3.81737 °/min
Orbital period
94.31 mins
BSTAR
0.00062895
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Other satellites on launch #207 in the year 2024 (2024-11-11 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-32567 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. |
|---|---|---|---|---|---|---|---|
| 7 mins | 2026-03-14 16:29:01.651Z | 253.62° W | 2026-03-14 16:33:01.651Z | 57.432° ENE | 43.126° | 2026-03-14 16:36:01.651Z | 71.31° E |
| 5 mins | 2026-03-14 18:10:01.651Z | 296.235° NW | 2026-03-14 18:12:01.651Z | 16.064° NNE | 37.555° | 2026-03-14 18:15:01.651Z | 76.129° E |
| 5 mins | 2026-03-14 19:49:01.651Z | 289.303° WNW | 2026-03-14 19:51:01.651Z | 81.523° E | 44.854° | 2026-03-14 19:54:01.651Z | 107.699° ESE |
| 4 mins | 2026-03-14 21:28:01.651Z | 249.672° W | 2026-03-14 21:30:01.651Z | 202.491° SSW | 21.509° | 2026-03-14 21:32:01.651Z | 165.524° S |
| 4 mins | 2026-03-15 14:25:01.651Z | 174.3° S | 2026-03-15 14:26:01.651Z | 149.638° SSE | 22.45° | 2026-03-15 14:29:01.651Z | 92.642° ESE |
| 5 mins | 2026-03-15 16:03:01.651Z | 254.49° W | 2026-03-15 16:05:01.651Z | 51.016° ENE | 44.43° | 2026-03-15 16:08:01.651Z | 71.342° 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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