ION SCV-011, 56957
Orbit data source: Space-Track
ION SCV-011, 56957 is a payload satellite owned by D-ORBIT (IT) in SSO that was launched on Mon, 12 Jun 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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56957 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: 10 hours ago
TLE from 10 hours ago
0 ION SCV-011
1 56957U 23084AB 26147.05527808 .00005955 00000-0 21695-3 0 9994
2 56957 98.1381 332.3814 0008540 108.8374 251.3790 15.28605493162588Epoch: 2026-05-27T01:19Z
TLE epoch observation values (Epoch: 2026-05-27T01:19:36.026Z)
Latitude
-0.00005°
Longitude
67.86144°
Altitude
484.935 km
Speed
7.622 km/s
True Right ascension
22h 09m 31s
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
20:33:04
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
482.822 km
Perigee altitude
471.113 km
Semi-major axis
6,855.104 km
Eccentricity
0.00085
Inclination
98.1381°
RAAN
332.3814°
Arg. of periapsis
108.8374°
True anomaly
251.28629°
Mean anomaly
251.379°
Eccentric anomaly
251.33264°
Mean motion
3.82404 °/min
Orbital period
94.14 mins
BSTAR
0.00021695
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Other satellites on launch #84 in the year 2023 (2023-06-12 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-011 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 | 2026-05-27 12:26:26.566Z | 171.399° S | 2026-05-27 12:29:26.566Z | 197.174° SSW | 41.348° | 2026-05-27 12:32:26.566Z | 341.714° N |
| 5 mins | 2026-05-28 01:27:26.566Z | 2.985° NNE | 2026-05-28 01:29:26.566Z | 326.289° NNW | 39.696° | 2026-05-28 01:32:26.566Z | 206.712° SW |
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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