ION SCV-010, 56192
Orbit data source: Space-Track
ION SCV-010, 56192 is a payload satellite owned by D-ORBIT (IT) in SSO that was launched on Sat, 15 Apr 2023 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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56192 intel report (Beta)
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Edit Public Description
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: 8 hours ago
TLE from 8 hours ago
0 ION SCV-010
1 56192U 23054Q 25310.25671141 .00008524 00000-0 36084-3 0 9998
2 56192 97.4017 197.5978 0011823 271.9152 88.0731 15.23361543142222Epoch: 2025-11-06T06:09Z
TLE epoch observation values (Epoch: 2025-11-06T06:09:39.865Z)
Latitude
-0.00003°
Longitude
59.46407°
Altitude
498.541 km
Speed
7.615 km/s
True Right ascension
13h 10m 23s
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
10:38:12
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
500.794 km
Perigee altitude
484.548 km
Semi-major axis
6,870.808 km
Eccentricity
0.00118
Inclination
97.4017°
RAAN
197.5978°
Arg. of periapsis
271.9152°
True anomaly
88.20851°
Mean anomaly
88.0731°
Eccentric anomaly
88.14081°
Mean motion
3.81093 °/min
Orbital period
94.47 mins
BSTAR
0.00036084
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Other satellites on launch #54 in the year 2023 (2023-04-15 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-010 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. |
|---|---|---|---|---|---|---|---|
| 4 mins | 2025-11-06 15:46:25.512Z | 107.791° ESE | 2025-11-06 15:48:25.512Z | 71.624° E | 17.182° | 2025-11-06 15:50:25.512Z | 33.287° NE |
| 4 mins | 2025-11-06 17:20:25.512Z | 223.694° SW | 2025-11-06 17:22:25.512Z | 275.283° WNW | 23.658° | 2025-11-06 17:24:25.512Z | 315.297° NNW |
| 4 mins | 2025-11-07 04:49:25.512Z | 59.144° ENE | 2025-11-07 04:51:25.512Z | 108.38° ESE | 21.95° | 2025-11-07 04:53:25.512Z | 146.195° SSE |
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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