STARLINK-32426, 61681
Orbit data source: Space-Track
STARLINK-32426, 61681 is a payload satellite owned by SpaceX/Seattle (US) in LEO that was launched on Sat, 26 Oct 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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61681 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: 13 hours ago
TLE from 13 hours ago
0 STARLINK-32426
1 61681U 24193W 26068.50230905 -.00002193 00000-0 -61998-4 0 9991
2 61681 53.1606 92.1809 0001259 78.0470 282.0672 15.30175538 76498Epoch: 2026-03-09T12:03Z
TLE epoch observation values (Epoch: 2026-03-09T12:03:19.501Z)
Latitude
-0.00003°
Longitude
104.15529°
Altitude
476.008 km
Speed
7.629 km/s
True Right ascension
06h 08m 43s
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
04:45:56
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
476.407 km
Perigee altitude
474.682 km
Semi-major axis
6,853.681 km
Eccentricity
0.00013
Inclination
53.1606°
RAAN
92.1809°
Arg. of periapsis
78.047°
True anomaly
282.05309°
Mean anomaly
282.0672°
Eccentric anomaly
282.06015°
Mean motion
3.82523 °/min
Orbital period
94.11 mins
BSTAR
-0.000061998
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Other satellites on launch #193 in the year 2024 (2024-10-26 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-32426 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 | 2026-03-10 03:53:35.105Z | 211.877° SW | 2026-03-10 03:56:35.105Z | 156.217° SSE | 37.93° | 2026-03-10 03:59:35.105Z | 62.251° ENE |
| 4 mins | 2026-03-10 05:33:35.105Z | 299.368° NW | 2026-03-10 05:34:35.105Z | 322.331° NNW | 21.652° | 2026-03-10 05:37:35.105Z | 24.632° NE |
| 5 mins | 2026-03-10 10:29:35.105Z | 327.969° NNW | 2026-03-10 10:31:35.105Z | 18.616° NNE | 35.285° | 2026-03-10 10:34:35.105Z | 105.254° ESE |
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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