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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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: 11 hours ago
TLE from 11 hours ago
0 ION SCV-011
1 56957U 23084AB 25346.98809802 .00008993 00000-0 34854-3 0 9999
2 56957 98.1269 152.4091 0007028 332.9612 27.1257 15.26394770137384Epoch: 2025-12-12T23:42Z
TLE epoch observation values (Epoch: 2025-12-12T23:42:51.668Z)
Latitude
-0.00009°
Longitude
74.772°
Altitude
485.384 km
Speed
7.625 km/s
True Right ascension
10h 09m 38s
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
09:16:24
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
488.413 km
Perigee altitude
478.768 km
Semi-major axis
6,861.727 km
Eccentricity
0.0007
Inclination
98.1269°
RAAN
152.4091°
Arg. of periapsis
332.9612°
True anomaly
27.16245°
Mean anomaly
27.1257°
Eccentric anomaly
27.14407°
Mean motion
3.8185 °/min
Orbital period
94.28 mins
BSTAR
0.00034854
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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 | 2025-12-13 10:51:22.246Z | 145.113° SSE | 2025-12-13 10:54:22.246Z | 79.384° E | 35.303° | 2025-12-13 10:57:22.246Z | 2.723° NNE |
| 5 mins | 2025-12-13 23:53:22.246Z | 28.693° NE | 2025-12-13 23:55:22.246Z | 84.866° E | 39.127° | 2025-12-13 23:58:22.246Z | 177.202° S |
| 4 mins | 2025-12-14 10:29:22.246Z | 103.698° ESE | 2025-12-14 10:30:22.246Z | 81.685° E | 20.506° | 2025-12-14 10:33:22.246Z | 19.72° NNE |
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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