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, 2.0 m
Radar Cross Section
0.240 m², Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 17 hours ago
TLE from 17 hours ago
0 ION SCV-011
1 56957U 23084AB 26260.26188373 .00004034 00000-0 14360-3 0 9991
2 56957 98.1360 96.1355 0008446 79.0895 281.1294 15.29606999179886Epoch: 2026-09-17T06:17Z
TLE epoch observation values (Epoch: 2026-09-17T06:17:06.754Z)
Latitude
0.00008°
Longitude
5.65569°
Altitude
478.954 km
Speed
7.627 km/s
True Right ascension
06h 24m 32s
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
16:10:06
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
479.759 km
Perigee altitude
468.185 km
Semi-major axis
6,852.109 km
Eccentricity
0.00084
Inclination
98.136°
RAAN
96.1355°
Arg. of periapsis
79.0895°
True anomaly
281.03442°
Mean anomaly
281.1294°
Eccentric anomaly
281.08191°
Mean motion
3.82654 °/min
Orbital period
94.08 mins
BSTAR
0.0001436
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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 | 2026-09-18 01:40:57.786Z | 28.427° NE | 2026-09-18 01:43:57.786Z | 86.423° E | 39.696° | 2026-09-18 01:46:57.786Z | 167.198° S |
| 4 mins | 2026-09-18 13:49:57.786Z | 226.773° WSW | 2026-09-18 13:50:57.786Z | 252.421° W | 25.776° | 2026-09-18 13:53:57.786Z | 318.263° NNW |
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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