ION SCV-007, 55060
Orbit data source: Space-Track
ION SCV-007, 55060 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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55060 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, Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 10 hours ago
TLE from 10 hours ago
0 ION SCV-007
1 55060U 23001BD 25345.19244373 .00000896 00000-0 13332-3 0 9992
2 55060 97.9286 46.7048 0011518 218.4949 141.5441 14.77317339158493Epoch: 2025-12-11T04:37Z
TLE epoch observation values (Epoch: 2025-12-11T04:37:07.138Z)
Latitude
0.00001°
Longitude
-102.72689°
Altitude
647.155 km
Speed
7.531 km/s
True Right ascension
03h 06m 49s
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
13:16:08
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
642.928 km
Perigee altitude
626.773 km
Semi-major axis
7,012.988 km
Eccentricity
0.00115
Inclination
97.9286°
RAAN
46.7048°
Arg. of periapsis
218.4949°
True anomaly
141.62609°
Mean anomaly
141.5441°
Eccentric anomaly
141.58511°
Mean motion
3.69563 °/min
Orbital period
97.41 mins
BSTAR
0.00013332
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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-007 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. |
|---|---|---|---|---|---|---|---|
| 7 mins | 2025-12-11 16:34:19.154Z | 32.553° NE | 2025-12-11 16:38:19.154Z | 106.622° ESE | 29.982° | 2025-12-11 16:41:19.154Z | 159.738° S |
| 5 mins | 2025-12-11 18:12:19.154Z | 326.026° NNW | 2025-12-11 18:14:19.154Z | 291.859° WNW | 19.005° | 2025-12-11 18:17:19.154Z | 247.379° WSW |
| 5 mins | 2025-12-12 03:32:19.154Z | 109.007° ESE | 2025-12-12 03:34:19.154Z | 66.567° ENE | 25.621° | 2025-12-12 03:37:19.154Z | 15.551° NNE |
| 5 mins | 2025-12-12 05:08:19.154Z | 222.616° SW | 2025-12-12 05:10:19.154Z | 258.038° W | 22.687° | 2025-12-12 05:13:19.154Z | 311.478° NW |
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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