ION SCV-008, 55051
Orbit data source: Space-Track
ION SCV-008, 55051 is a payload satellite owned by D-ORBIT (IT) in SSO that was launched on Tue, 03 Jan 2023 UTC via an FALCON 9 launch vehicle from the Air Force Eastern Test Range (AFETR). 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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55051 intel report (Beta)
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Identifier
Orbit
Country
ITRelated business
Manufacturer
D-ORBIT
Mission
Operational Commercial Technology
Bus & Motor
ION-SC, PM200
Mass
220 kg wet, 150 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Box, 0.2 m
Radar Cross Section
0.240 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 7 hours ago
TLE from 7 hours ago
0 ION SCV-008
1 55051U 23001AU 26115.52905347 .00007442 00000-0 27525-3 0 9993
2 55051 97.5674 211.0036 0014915 192.8111 167.2751 15.27897853183299Epoch: 2026-04-25T12:41Z
TLE epoch observation values (Epoch: 2026-04-25T12:41:50.219Z)
Latitude
-0.00006°
Longitude
166.99824°
Altitude
495.178 km
Speed
7.612 km/s
True Right ascension
14h 04m 00s
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
03:04:06
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
489.287 km
Perigee altitude
468.832 km
Semi-major axis
6,857.197 km
Eccentricity
0.00149
Inclination
97.5674°
RAAN
211.0036°
Arg. of periapsis
192.8111°
True anomaly
167.31268°
Mean anomaly
167.2751°
Eccentric anomaly
167.2939°
Mean motion
3.82229 °/min
Orbital period
94.18 mins
BSTAR
0.00027525
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Other satellites on launch #1 in the year 2023 (2023-01-03 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.ION SCV-008 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 | 2026-04-26 06:07:13.989Z | 149.679° SSE | 2026-04-26 06:10:13.989Z | 54.774° ENE | 38.715° | 2026-04-26 06:13:13.989Z | 357.899° N |
| 5 mins | 2026-04-26 19:08:13.989Z | 18.862° NNE | 2026-04-26 19:10:13.989Z | 82.964° E | 43.908° | 2026-04-26 19:13:13.989Z | 186.909° SSW |
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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