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: 6 hours ago
TLE from 6 hours ago
0 ION SCV-007
1 55060U 23001BD 25336.18410639 .00000734 00000-0 11061-3 0 9999
2 55060 97.9297 37.8492 0011143 250.4096 109.5912 14.77297370157164Epoch: 2025-12-02T04:25Z
TLE epoch observation values (Epoch: 2025-12-02T04:25:06.792Z)
Latitude
0.00003°
Longitude
-99.70201°
Altitude
643.515 km
Speed
7.535 km/s
True Right ascension
02h 31m 23s
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
07:42:58
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
642.728 km
Perigee altitude
627.099 km
Semi-major axis
7,013.051 km
Eccentricity
0.00111
Inclination
97.9297°
RAAN
37.8492°
Arg. of periapsis
250.4096°
True anomaly
109.71144°
Mean anomaly
109.5912°
Eccentric anomaly
109.65133°
Mean motion
3.69558 °/min
Orbital period
97.41 mins
BSTAR
0.00011061
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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 | 2025-12-02 16:22:26.842Z | 38.146° NE | 2025-12-02 16:26:26.842Z | 103.455° ESE | 24.009° | 2025-12-02 16:29:26.842Z | 150.615° SSE |
| 5 mins | 2025-12-02 18:00:26.842Z | 331.308° NNW | 2025-12-02 18:02:26.842Z | 292.333° WNW | 24.015° | 2025-12-02 18:05:26.842Z | 240.639° WSW |
| 5 mins | 2025-12-03 03:20:26.842Z | 102.379° ESE | 2025-12-03 03:22:26.842Z | 67.241° ENE | 20.512° | 2025-12-03 03:25:26.842Z | 20.728° NNE |
| 6 mins | 2025-12-03 04:56:26.842Z | 213.631° SW | 2025-12-03 04:58:26.842Z | 255.625° W | 28.532° | 2025-12-03 05:02:26.842Z | 326.073° NNW |
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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