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: 10 hours ago
TLE from 10 hours ago
0 STARLINK-32426
1 61681U 24193W 26171.43838397 -.00000353 00000-0 21944-6 0 9991
2 61681 53.1616 334.0523 0001441 91.4492 268.6674 15.30186673 92252Epoch: 2026-06-20T10:31Z
TLE epoch observation values (Epoch: 2026-06-20T10:31:16.375Z)
Latitude
0.00001°
Longitude
-92.41892°
Altitude
476.178 km
Speed
7.629 km/s
True Right ascension
22h 16m 12s
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
07:22:49
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
476.499 km
Perigee altitude
474.523 km
Semi-major axis
6,853.648 km
Eccentricity
0.00014
Inclination
53.1616°
RAAN
334.0523°
Arg. of periapsis
91.4492°
True anomaly
268.65089°
Mean anomaly
268.6674°
Eccentric anomaly
268.65915°
Mean motion
3.82526 °/min
Orbital period
94.11 mins
BSTAR
2.1944e-7
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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. |
|---|---|---|---|---|---|---|---|
| 4 mins | 2026-06-20 20:27:02.865Z | 322.408° NNW | 2026-06-20 20:28:02.865Z | 358.529° N | 43.093° | 2026-06-20 20:31:02.865Z | 122.993° SE |
| 5 mins | 2026-06-21 13:22:02.865Z | 219.335° SW | 2026-06-21 13:24:02.865Z | 90.895° ESE | 43.277° | 2026-06-21 13:27:02.865Z | 53.179° ENE |
| 5 mins | 2026-06-21 19:57:02.865Z | 324.182° NNW | 2026-06-21 19:59:02.865Z | 60.522° ENE | 41.246° | 2026-06-21 20:02:02.865Z | 118.817° 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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