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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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, 0.3 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-007
1 55060U 23001BD 26296.11808149 .00000331 00000-0 53366-4 0 9993
2 55060 97.8856 356.4940 0010972 283.8692 76.1297 14.77643767205145Epoch: 2026-10-23T02:50Z
TLE epoch observation values (Epoch: 2026-10-23T02:50:02.240Z)
Latitude
-0.00012°
Longitude
-77.55854°
Altitude
637.953 km
Speed
7.54 km/s
True Right ascension
23h 45m 58s
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
15:43:37
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
641.508 km
Perigee altitude
626.121 km
Semi-major axis
7,011.952 km
Eccentricity
0.0011
Inclination
97.8856°
RAAN
356.494°
Arg. of periapsis
283.8692°
True anomaly
76.2518°
Mean anomaly
76.1297°
Eccentric anomaly
76.19075°
Mean motion
3.69645 °/min
Orbital period
97.39 mins
BSTAR
0.000053366
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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 | 2026-10-24 03:21:00.840Z | 122.555° SE | 2026-10-24 03:24:00.840Z | 76.7° E | 26.084° | 2026-10-24 03:28:00.840Z | 12.635° NNE |
| 6 mins | 2026-10-24 04:58:00.840Z | 215.329° SW | 2026-10-24 05:01:00.840Z | 271.608° WNW | 26.895° | 2026-10-24 05:04:00.840Z | 319.1° NNW |
| 7 mins | 2026-10-24 16:48:00.840Z | 26.015° NE | 2026-10-24 16:51:00.840Z | 112.621° SE | 59.409° | 2026-10-24 16:55:00.840Z | 180.57° SSW |
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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