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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Edit Public Description
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: 13 hours ago
TLE from 13 hours ago
0 SEDNA-1
1 60580U 24149DS 25289.21368593 .00008330 00000-0 62709-3 0 9993
2 60580 97.6881 6.2004 0011380 99.1157 261.1356 15.02718064 63699Epoch: 2025-10-16T05:07Z
TLE epoch observation values (Epoch: 2025-10-16T05:07:42.464Z)
Latitude
-0.00001°
Longitude
-95.70316°
Altitude
562.803 km
Speed
7.579 km/s
True Right ascension
00h 24m 48s
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
12:35:07
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
563.411 km
Perigee altitude
547.63 km
Semi-major axis
6,933.657 km
Eccentricity
0.00114
Inclination
97.6881°
RAAN
6.2004°
Arg. of periapsis
99.1157°
True anomaly
261.00678°
Mean anomaly
261.1356°
Eccentric anomaly
261.07119°
Mean motion
3.75924 °/min
Orbital period
95.76 mins
BSTAR
0.00062709
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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 | 2025-10-16 18:28:35.489Z | 357.608° N | 2025-10-16 18:31:35.489Z | 288.91° WNW | 37.144° | 2025-10-16 18:34:35.489Z | 215.174° SW |
| 6 mins | 2025-10-17 05:14:35.489Z | 162.678° S | 2025-10-17 05:16:35.489Z | 122.748° SE | 44.613° | 2025-10-17 05:20:35.489Z | 349.36° N |
Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
Click to sort rows by RSO header in ascending order | Click to sort rows by Country header in ascending order | Click to sort rows by Type header in ascending order | Click to sort rows by Inclination Δ header in ascending order | Click to sort rows by RAAN Δ header in ascending order | Click to sort rows by Coplanar Angle header in ascending order | Click to sort rows by SMA Δ header in ascending order | Click to sort rows by Orbital period header in ascending order | Click to sort rows by <5km Md TCA header in ascending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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