STARLINK-32450, 61969
Orbit data source: Space-Track
STARLINK-32450, 61969 is a payload satellite owned by SpaceX/Seattle (US) in LEO that was launched on Thu, 14 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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61969 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: 10 hours ago
TLE from 10 hours ago
0 STARLINK-32450
1 61969U 24210L 26171.42047429 .00016799 00000-0 61838-3 0 9990
2 61969 43.0027 312.5346 0002010 275.4780 84.5842 15.27590797 90573Epoch: 2026-06-20T10:05Z
TLE epoch observation values (Epoch: 2026-06-20T10:05:28.978Z)
Latitude
-0.00005°
Longitude
-107.47155°
Altitude
482.663 km
Speed
7.626 km/s
True Right ascension
20h 50m 08s
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
07:17:26
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
486.341 km
Perigee altitude
483.582 km
Semi-major axis
6,863.098 km
Eccentricity
0.0002
Inclination
43.0027°
RAAN
312.5346°
Arg. of periapsis
275.478°
True anomaly
84.60713°
Mean anomaly
84.5842°
Eccentric anomaly
84.59567°
Mean motion
3.81736 °/min
Orbital period
94.31 mins
BSTAR
0.00061838
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Other satellites on launch #210 in the year 2024 (2024-11-14 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-32450 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 | 2026-06-21 13:00:41.379Z | 225.273° WSW | 2026-06-21 13:02:41.379Z | 151.106° SSE | 40.065° | 2026-06-21 13:05:41.379Z | 78.409° E |
| 5 mins | 2026-06-21 14:39:41.379Z | 282.358° WNW | 2026-06-21 14:41:41.379Z | 356.984° N | 39.784° | 2026-06-21 14:44:41.379Z | 69.705° E |
| 5 mins | 2026-06-21 16:18:41.379Z | 295.529° NW | 2026-06-21 16:20:41.379Z | 355.589° N | 41.007° | 2026-06-21 16:23:41.379Z | 89.042° E |
| 5 mins | 2026-06-21 17:57:41.379Z | 270.54° WNW | 2026-06-21 17:59:41.379Z | 211.38° SW | 35.657° | 2026-06-21 18:02:41.379Z | 136.962° SSE |
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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