ION SCV-002, 47504
Orbit data source: Space-Track
ION SCV-002, 47504 is a payload satellite owned by D-ORBIT (IT) in SSO that was launched on Sun, 24 Jan 2021 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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47504 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, Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 8 hours ago
TLE from 8 hours ago
0 ION SCV-002
1 47504U 21006CV 25289.08747419 .00015512 00000-0 43107-3 0 9997
2 47504 97.1146 292.5523 0010518 286.2710 73.7378 15.36894740262449Epoch: 2025-10-16T02:05Z
TLE epoch observation values (Epoch: 2025-10-16T02:05:57.770Z)
Latitude
0.00002°
Longitude
-123.79064°
Altitude
456.414 km
Speed
7.64 km/s
True Right ascension
19h 30m 12s
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
04:27:33
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
459.414 km
Perigee altitude
445.045 km
Semi-major axis
6,830.366 km
Eccentricity
0.00105
Inclination
97.1146°
RAAN
292.5523°
Arg. of periapsis
286.271°
True anomaly
73.85355°
Mean anomaly
73.7378°
Eccentric anomaly
73.79567°
Mean motion
3.84483 °/min
Orbital period
93.63 mins
BSTAR
0.00043107
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Other satellites on launch #6 in the year 2021 (2021-01-24 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-002 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. |
|---|---|---|---|---|---|---|---|
| 6 mins | 2025-10-16 13:35:21.645Z | 355.083° N | 2025-10-16 13:38:21.645Z | 286.661° WNW | 32.896° | 2025-10-16 13:41:21.645Z | 216.673° SW |
| 5 mins | 2025-10-17 00:07:21.645Z | 139.553° SSE | 2025-10-17 00:09:21.645Z | 65.752° ENE | 36.34° | 2025-10-17 00:12:21.645Z | 0.949° NNE |
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 ascending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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