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, 0.2 m
Radar Cross Section
0.035 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 8 hours ago
TLE from 8 hours ago
0 SEDNA-1
1 60580U 24149DS 26265.17875328 .00004892 00000-0 32113-3 0 9997
2 60580 97.6575 345.2724 0009057 25.8706 334.2973 15.08080953115003Epoch: 2026-09-22T04:17Z
TLE epoch observation values (Epoch: 2026-09-22T04:17:24.283Z)
Latitude
-0.00003°
Longitude
-80.12673°
Altitude
539.484 km
Speed
7.596 km/s
True Right ascension
23h 01m 05s
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
05:26:55
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
545.322 km
Perigee altitude
532.792 km
Semi-major axis
6,917.194 km
Eccentricity
0.00091
Inclination
97.6575°
RAAN
345.2724°
Arg. of periapsis
25.8706°
True anomaly
334.25224°
Mean anomaly
334.2973°
Eccentric anomaly
334.27478°
Mean motion
3.77266 °/min
Orbital period
95.42 mins
BSTAR
0.00032113
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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. |
|---|---|---|---|---|---|---|---|
| 6 mins | 2026-09-22 17:35:53.076Z | 39.042° NE | 2026-09-22 17:38:53.076Z | 88.947° E | 25.037° | 2026-09-22 17:41:53.076Z | 147.671° SSE |
| 4 mins | 2026-09-22 19:11:53.076Z | 325.663° NNW | 2026-09-22 19:13:53.076Z | 284.056° WNW | 21.804° | 2026-09-22 19:15:53.076Z | 247.921° W |
| 6 mins | 2026-09-23 05:53:53.076Z | 195.636° SSW | 2026-09-23 05:56:53.076Z | 277.406° WNW | 41.058° | 2026-09-23 05:59:53.076Z | 331.697° NNW |
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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