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: 9 hours ago
TLE from 9 hours ago
0 SEDNA-1
1 60580U 24149DS 26219.78790988 .00003542 00000-0 23646-3 0 9993
2 60580 97.6607 300.0524 0009593 164.9064 195.2452 15.07639373108164Epoch: 2026-08-07T18:54Z
TLE epoch observation values (Epoch: 2026-08-07T18:54:35.413Z)
Latitude
-0.00001°
Longitude
60.09626°
Altitude
552.89 km
Speed
7.582 km/s
True Right ascension
20h 00m 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
17:39:14
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
547.046 km
Perigee altitude
533.772 km
Semi-major axis
6,918.546 km
Eccentricity
0.00096
Inclination
97.6607°
RAAN
300.0524°
Arg. of periapsis
164.9064°
True anomaly
195.21633°
Mean anomaly
195.2452°
Eccentric anomaly
195.23076°
Mean motion
3.77156 °/min
Orbital period
95.45 mins
BSTAR
0.00023646
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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 | 2026-08-08 04:37:04.084Z | 113.524° SE | 2026-08-08 04:39:04.084Z | 78.342° E | 20.303° | 2026-08-08 04:42:04.084Z | 22.23° NNE |
| 5 mins | 2026-08-08 06:12:04.084Z | 223.72° SW | 2026-08-08 06:14:04.084Z | 267.64° W | 22.845° | 2026-08-08 06:17:04.084Z | 319.665° NNW |
| 5 mins | 2026-08-08 17:48:04.084Z | 47.244° ENE | 2026-08-08 17:50:04.084Z | 102.216° ESE | 29.716° | 2026-08-08 17:53:04.084Z | 162.019° S |
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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