SEDNA-2, 63153
Orbit data source: Space-Track
SEDNA-2, 63153 is a payload satellite owned by AAC ClydeSpace (US) in SSO that was launched on Tue, 14 Jan 2025 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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63153 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 1X4U, Unknown motor
Mass
~10 kg wet, ~10 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Box, 0.4 m
Radar Cross Section
0.045 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 6 hours ago
TLE from 6 hours ago
0 SEDNA-2
1 63153U 25009DQ 25290.96913425 .00018649 00000-0 12317-2 0 9995
2 63153 97.4823 5.6943 0010363 170.1890 189.9543 15.07419975 41573Epoch: 2025-10-17T23:15Z
TLE epoch observation values (Epoch: 2025-10-17T23:15:33.199Z)
Latitude
0.00006°
Longitude
-9.90092°
Altitude
554.226 km
Speed
7.581 km/s
True Right ascension
00h 22m 46s
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
00:16:37
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
548.244 km
Perigee altitude
533.903 km
Semi-major axis
6,919.21 km
Eccentricity
0.00104
Inclination
97.4823°
RAAN
5.6943°
Arg. of periapsis
170.189°
True anomaly
189.9338°
Mean anomaly
189.9543°
Eccentric anomaly
189.94405°
Mean motion
3.77102 °/min
Orbital period
95.46 mins
BSTAR
0.0012317
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Other satellites on launch #9 in the year 2025 (2025-01-14 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-2 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 | 2025-10-18 05:45:14.886Z | 203.996° SW | 2025-10-18 05:48:14.886Z | 262.291° W | 26.759° | 2025-10-18 05:51:14.886Z | 321.939° NNW |
| 5 mins | 2025-10-18 17:22:14.886Z | 47.248° ENE | 2025-10-18 17:24:14.886Z | 92.383° ESE | 26.276° | 2025-10-18 17:27:14.886Z | 154.416° SSE |
| 4 mins | 2025-10-18 18:57:14.886Z | 321.115° NNW | 2025-10-18 18:59:14.886Z | 282.658° WNW | 17.066° | 2025-10-18 19:01:14.886Z | 250.375° 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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