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: 7 hours ago
TLE from 7 hours ago
0 ION SCV-011
1 56957U 23084AB 26136.25392856 .00004119 00000-0 15153-3 0 9990
2 56957 98.1377 320.5840 0008109 141.3575 218.8244 15.28511449160933Epoch: 2026-05-16T06:05Z
TLE epoch observation values (Epoch: 2026-05-16T06:05:39.427Z)
Latitude
-0.00005°
Longitude
-4.80381°
Altitude
487.677 km
Speed
7.619 km/s
True Right ascension
21h 22m 20s
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
21:39:06
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
482.808 km
Perigee altitude
471.69 km
Semi-major axis
6,855.386 km
Eccentricity
0.00081
Inclination
98.1377°
RAAN
320.584°
Arg. of periapsis
141.3575°
True anomaly
218.76619°
Mean anomaly
218.8244°
Eccentric anomaly
218.79529°
Mean motion
3.8238 °/min
Orbital period
94.15 mins
BSTAR
0.00015153
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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. |
|---|---|---|---|---|---|---|---|
| 5 mins | 2026-05-17 01:30:32.614Z | 357.164° N | 2026-05-17 01:33:32.614Z | 262.613° W | 35.494° | 2026-05-17 01:35:32.614Z | 217.051° SW |
| 5 mins | 2026-05-17 12:05:32.614Z | 146.804° SSE | 2026-05-17 12:07:32.614Z | 67.999° E | 40.641° | 2026-05-17 12:10:32.614Z | 356.198° N |
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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