ION SCV-008, 55051
Orbit data source: Space-Track
ION SCV-008, 55051 is a payload satellite owned by D-ORBIT (IT) in SSO that was launched on Tue, 03 Jan 2023 UTC via an FALCON 9 launch vehicle from the Air Force Eastern Test Range (AFETR). 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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55051 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: 18 hours ago
TLE from 18 hours ago
0 ION SCV-008
1 55051U 23001AU 26206.52813149 .00006180 00000-0 22182-3 0 9994
2 55051 97.5717 303.4998 0013562 232.8615 127.1387 15.28982000197195Epoch: 2026-07-25T12:40Z
TLE epoch observation values (Epoch: 2026-07-25T12:40:30.560Z)
Latitude
0.00003°
Longitude
170.13334°
Altitude
487.576 km
Speed
7.618 km/s
True Right ascension
20h 13m 59s
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
20:21:16
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
485.111 km
Perigee altitude
466.52 km
Semi-major axis
6,853.952 km
Eccentricity
0.00136
Inclination
97.5717°
RAAN
303.4998°
Arg. of periapsis
232.8615°
True anomaly
127.26246°
Mean anomaly
127.1387°
Eccentric anomaly
127.20059°
Mean motion
3.825 °/min
Orbital period
94.12 mins
BSTAR
0.00022182
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Other satellites on launch #1 in the year 2023 (2023-01-03 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-008 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 | 2026-07-26 19:05:46.295Z | 33.624° NE | 2026-07-26 19:07:46.295Z | 94.121° ESE | 35.998° | 2026-07-26 19:10:46.295Z | 172.187° S |
| 4 mins | 2026-07-27 05:39:46.295Z | 110.455° ESE | 2026-07-27 05:41:46.295Z | 75.826° E | 16.752° | 2026-07-27 05:43:46.295Z | 35.841° NE |
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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Click to sort rows by Secondary header in ascending order | Click to sort rows by Secondary name header in ascending order | Click to sort rows by Country header in ascending order | Click to sort rows by Owner header in ascending order | Click to sort rows by Obj. Type header in ascending order | Click to sort rows by Miss dist. header in ascending order | Click to sort rows by Rel. speed header in ascending order | Click to sort rows by Apr. angle header in ascending order | Click to sort rows by TCA header in descending order |
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