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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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, 2.0 m
Radar Cross Section
0.240 m², Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 16 hours ago
TLE from 16 hours ago
0 ION SCV-010
1 56192U 23054Q 26303.62980770 .00003567 00000-0 12960-3 0 9992
2 56192 97.3573 191.4973 0013344 58.0400 302.2135 15.28859484196876Epoch: 2026-10-30T15:06Z
TLE epoch observation values (Epoch: 2026-10-30T15:06:55.385Z)
Latitude
-0.00006°
Longitude
-74.1806°
Altitude
477.454 km
Speed
7.63 km/s
True Right ascension
12h 45m 59s
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
02:17:38
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
485.319 km
Perigee altitude
467.026 km
Semi-major axis
6,854.309 km
Eccentricity
0.00133
Inclination
97.3573°
RAAN
191.4973°
Arg. of periapsis
58.04°
True anomaly
302.08401°
Mean anomaly
302.2135°
Eccentric anomaly
302.14877°
Mean motion
3.8247 °/min
Orbital period
94.12 mins
BSTAR
0.0001296
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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. |
|---|---|---|---|---|---|---|---|
| 6 mins | 2026-10-31 16:22:45.987Z | 144.972° SSE | 2026-10-31 16:25:45.987Z | 65.922° ENE | 44.748° | 2026-10-31 16:28:45.987Z | 2.123° NNE |
| 5 mins | 2026-11-01 05:23:45.987Z | 26.483° NE | 2026-11-01 05:25:45.987Z | 132.339° SE | 61.187° | 2026-11-01 05:28:45.987Z | 183.049° 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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Click to sort rows by Secondary header in ascending order | Click to sort rows by Secondary name header in ascending order | Click to sort rows by Country header in ascending order | Click to sort rows by Owner header in ascending order | Click to sort rows by Obj. Type header in ascending order | Click to sort rows by Miss dist. header in ascending order | Click to sort rows by Rel. speed header in ascending order | Click to sort rows by Apr. angle header in ascending order | Click to sort rows by TCA header in descending order |
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