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: 1 day ago
TLE from 1 day ago
0 ION SCV-011
1 56957U 23084AB 26041.42872847 .00007036 00000-0 26559-3 0 9990
2 56957 98.1321 217.1110 0008493 114.2765 245.9359 15.27355657146454Epoch: 2026-02-10T10:17Z
TLE epoch observation values (Epoch: 2026-02-10T10:17:22.139Z)
Latitude
-0.00014°
Longitude
-77.74055°
Altitude
489.18 km
Speed
7.619 km/s
True Right ascension
14h 28m 26s
True Declination
0° 00' 01"
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
15:01:48
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
486.535 km
Perigee altitude
474.884 km
Semi-major axis
6,858.847 km
Eccentricity
0.00085
Inclination
98.1321°
RAAN
217.111°
Arg. of periapsis
114.2765°
True anomaly
245.84707°
Mean anomaly
245.9359°
Eccentric anomaly
245.89148°
Mean motion
3.82091 °/min
Orbital period
94.22 mins
BSTAR
0.00026559
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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 | 2026-02-12 00:34:55.532Z | 10.629° NNE | 2026-02-12 00:37:55.532Z | 308.04° NW | 44.649° | 2026-02-12 00:40:55.532Z | 197.206° SSW |
| 5 mins | 2026-02-12 11:10:55.532Z | 126.895° SE | 2026-02-12 11:12:55.532Z | 67.346° ENE | 30.645° | 2026-02-12 11:15:55.532Z | 5.499° 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 descending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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