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, Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 11 hours ago
TLE from 11 hours ago
0 ION SCV-011
1 56957U 23084AB 26197.12359947 .00002684 00000-0 98147-4 0 9997
2 56957 98.1377 27.0897 0005930 302.0928 57.9734 15.29101711170239Epoch: 2026-07-16T02:57Z
TLE epoch observation values (Epoch: 2026-07-16T02:57:58.994Z)
Latitude
0.00002°
Longitude
48.62432°
Altitude
479.422 km
Speed
7.627 km/s
True Right ascension
01h 48m 21s
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
02:08:23
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
479.547 km
Perigee altitude
471.419 km
Semi-major axis
6,853.62 km
Eccentricity
0.00059
Inclination
98.1377°
RAAN
27.0897°
Arg. of periapsis
302.0928°
True anomaly
58.03103°
Mean anomaly
57.9734°
Eccentric anomaly
58.00221°
Mean motion
3.82528 °/min
Orbital period
94.11 mins
BSTAR
0.000098147
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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 | 2026-07-17 01:31:15.283Z | 19.304° NNE | 2026-07-17 01:34:15.283Z | 152.877° SSE | 41.642° | 2026-07-17 01:37:15.283Z | 187.238° SSW |
| 4 mins | 2026-07-17 12:06:15.283Z | 113.014° SE | 2026-07-17 12:08:15.283Z | 60.89° ENE | 23.92° | 2026-07-17 12:10:15.283Z | 18.98° 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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