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: 21 hours ago
TLE from 21 hours ago
0 STARLINK-32426
1 61681U 24193W 26305.08113918 .00035815 00000-0 10653-2 0 9997
2 61681 53.1590 71.2578 0001145 63.7406 296.3715 15.34424546112740Epoch: 2026-11-01T01:56Z
TLE epoch observation values (Epoch: 2026-11-01T01:56:50.425Z)
Latitude
0.00006°
Longitude
1.67011°
Altitude
463.184 km
Speed
7.636 km/s
True Right ascension
04h 45m 01s
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
19:04:53
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
463.671 km
Perigee altitude
462.104 km
Semi-major axis
6,841.024 km
Eccentricity
0.00011
Inclination
53.159°
RAAN
71.2578°
Arg. of periapsis
63.7406°
True anomaly
296.35974°
Mean anomaly
296.3715°
Eccentric anomaly
296.36562°
Mean motion
3.83585 °/min
Orbital period
93.85 mins
BSTAR
0.0010653
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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 | 2026-11-02 10:57:19.997Z | 222.836° SW | 2026-11-02 11:00:19.997Z | 81.637° E | 68.058° | 2026-11-02 11:03:19.997Z | 52.68° ENE |
| 4 mins | 2026-11-02 12:36:19.997Z | 302.504° NW | 2026-11-02 12:38:19.997Z | 344.909° N | 19.135° | 2026-11-02 12:40:19.997Z | 20.725° NNE |
| 6 mins | 2026-11-02 17:31:19.997Z | 319.719° NNW | 2026-11-02 17:34:19.997Z | 74.119° E | 55.161° | 2026-11-02 17:37:19.997Z | 118.559° 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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