ION SCV-004, 50993
Orbit data source: Space-Track
ION SCV-004, 50993 is a payload satellite owned by D-ORBIT (IT) in SSO that was launched on Thu, 13 Jan 2022 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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50993 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: 6 hours ago
TLE from 6 hours ago
0 ION SCV-004
1 50993U 22002K 25291.15546080 .00009919 00000-0 37393-3 0 9996
2 50993 97.3217 348.3540 0009341 127.8266 232.3820 15.27221165208319Epoch: 2025-10-18T03:43Z
TLE epoch observation values (Epoch: 2025-10-18T03:43:51.813Z)
Latitude
-0.00001°
Longitude
-94.50242°
Altitude
491.144 km
Speed
7.617 km/s
True Right ascension
23h 13m 24s
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
04:26:15
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
487.484 km
Perigee altitude
474.669 km
Semi-major axis
6,859.213 km
Eccentricity
0.00093
Inclination
97.3217°
RAAN
348.354°
Arg. of periapsis
127.8266°
True anomaly
232.29727°
Mean anomaly
232.382°
Eccentric anomaly
232.33963°
Mean motion
3.8206 °/min
Orbital period
94.23 mins
BSTAR
0.00037393
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Other satellites on launch #2 in the year 2022 (2022-01-13 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-004 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 16:52:11.809Z | 8.588° NNE | 2025-10-18 16:55:11.809Z | 273.039° WNW | 44.423° | 2025-10-18 16:58:11.809Z | 197.325° SSW |
| 5 mins | 2025-10-19 03:28:11.809Z | 122.769° SE | 2025-10-19 03:30:11.809Z | 66.952° ENE | 27.978° | 2025-10-19 03:33:11.809Z | 8.668° NNE |
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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