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 26034.27779869 .00009146 00000-0 56790-3 0 9994
2 63153 97.4686 111.1601 0010050 157.7262 202.4406 15.09865584 57907Epoch: 2026-02-03T06:40Z
TLE epoch observation values (Epoch: 2026-02-03T06:40:01.806Z)
Latitude
-0.00003°
Longitude
-122.30845°
Altitude
546.111 km
Speed
7.586 km/s
True Right ascension
07h 24m 38s
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
14:56:45
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
540.539 km
Perigee altitude
526.646 km
Semi-major axis
6,911.729 km
Eccentricity
0.00101
Inclination
97.4686°
RAAN
111.1601°
Arg. of periapsis
157.7262°
True anomaly
202.39669°
Mean anomaly
202.4406°
Eccentric anomaly
202.41864°
Mean motion
3.77714 °/min
Orbital period
95.31 mins
BSTAR
0.0005679
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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. |
|---|---|---|---|---|---|---|---|
| 5 mins | 2026-02-03 18:22:20.117Z | 346.394° N | 2026-02-03 18:24:20.117Z | 301.136° NW | 31.126° | 2026-02-03 18:27:20.117Z | 224.855° SW |
| 6 mins | 2026-02-04 05:04:20.117Z | 167.904° S | 2026-02-04 05:06:20.117Z | 171.874° S | 43.28° | 2026-02-04 05:10:20.117Z | 347.626° 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 descending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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