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: 13 hours ago
TLE from 13 hours ago
0 ION SCV-007
1 55060U 23001BD 26024.14913053 .00001233 00000-0 18034-3 0 9990
2 55060 97.9215 89.9007 0013743 82.4821 277.7950 14.77390007164980Epoch: 2026-01-24T03:34Z
TLE epoch observation values (Epoch: 2026-01-24T03:34:44.877Z)
Latitude
-0.00006°
Longitude
-87.26402°
Altitude
639.297 km
Speed
7.539 km/s
True Right ascension
05h 59m 36s
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
17:27:40
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
644.258 km
Perigee altitude
624.982 km
Semi-major axis
7,012.757 km
Eccentricity
0.00137
Inclination
97.9215°
RAAN
89.9007°
Arg. of periapsis
82.4821°
True anomaly
277.63894°
Mean anomaly
277.795°
Eccentric anomaly
277.71697°
Mean motion
3.69581 °/min
Orbital period
97.41 mins
BSTAR
0.00018034
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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 | 2026-01-24 17:09:10.255Z | 12.718° NNE | 2026-01-24 17:13:10.255Z | 192.436° SSW | 43.356° | 2026-01-24 17:16:10.255Z | 193.609° SSW |
| 6 mins | 2026-01-25 04:06:10.255Z | 152.677° SSE | 2026-01-25 04:09:10.255Z | 34.088° NE | 41.489° | 2026-01-25 04:12:10.255Z | 354.377° 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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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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