SEDNA-1, 60580
Orbit data source: Space-Track
SEDNA-1, 60580 is a payload satellite owned by AAC ClydeSpace (US) in SSO that was launched on Fri, 16 Aug 2024 UTC via an FALCON 9 launch vehicle from the Air Force Western Test Range (AFWTR). 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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60580 intel report (Beta)
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Identifier
Orbit
Country
USRelated business
Manufacturer
AAC ClydeSpace
Mission
Operational Commercial Communications
Bus & Motor
CUBESAT 3U, Unknown motor
Mass
4 kg wet, 4 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Box, 0.1 m
Radar Cross Section
0.035 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 1 day ago
TLE from 1 day ago
0 SEDNA-1
1 60580U 24149DS 26173.45298023 .00004984 00000-0 33618-3 0 9990
2 60580 97.6623 253.9030 0008021 336.7163 23.3700 15.07076077101182Epoch: 2026-06-22T10:52Z
TLE epoch observation values (Epoch: 2026-06-22T10:52:17.491Z)
Latitude
-0.00005°
Longitude
-179.80856°
Altitude
543.108 km
Speed
7.593 km/s
True Right ascension
16h 55m 36s
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
09:27:59
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
547.685 km
Perigee altitude
536.584 km
Semi-major axis
6,920.271 km
Eccentricity
0.0008
Inclination
97.6623°
RAAN
253.903°
Arg. of periapsis
336.7163°
True anomaly
23.40649°
Mean anomaly
23.37°
Eccentric anomaly
23.38824°
Mean motion
3.77015 °/min
Orbital period
95.49 mins
BSTAR
0.00033618
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Other satellites on launch #149 in the year 2024 (2024-08-16 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.SEDNA-1 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 | 2026-06-24 04:27:04.752Z | 110.483° ESE | 2026-06-24 04:30:04.752Z | 59.6° ENE | 17.016° | 2026-06-24 04:32:04.752Z | 27.167° NE |
| 5 mins | 2026-06-24 06:02:04.752Z | 214.727° SW | 2026-06-24 06:04:04.752Z | 263.005° W | 27.033° | 2026-06-24 06:07:04.752Z | 322.491° NNW |
| 5 mins | 2026-06-24 17:38:04.752Z | 46.551° ENE | 2026-06-24 17:40:04.752Z | 87.859° E | 25.486° | 2026-06-24 17:43:04.752Z | 151.367° SSE |
| 4 mins | 2026-06-24 19:13:04.752Z | 324.633° NNW | 2026-06-24 19:15:04.752Z | 286.167° WNW | 18.42° | 2026-06-24 19:17:04.752Z | 251.709° W |
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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