ION SCV-014, 62630
Orbit data source: Space-Track
ION SCV-014, 62630 is a payload satellite owned by D-ORBIT (IT) in SSO that was launched on Tue, 14 Jan 2025 UTC via an FALCON 9 launch vehicle from the Air Force Western Test Range (AFWTR). 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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62630 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, 1.1 m
Radar Cross Section
0.240 m², Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 9 hours ago
TLE from 9 hours ago
0 ION SCV-014
1 62630U 25009X 26238.17344671 .00000872 00000-0 64926-4 0 9995
2 62630 97.4805 309.2246 0003128 257.7198 102.3679 15.05411393 88513Epoch: 2026-08-26T04:09Z
TLE epoch observation values (Epoch: 2026-08-26T04:09:45.795Z)
Latitude
-0.00003°
Longitude
-87.64645°
Altitude
553.776 km
Speed
7.585 km/s
True Right ascension
20h 36m 53s
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
04:37:49
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
549.398 km
Perigee altitude
545.065 km
Semi-major axis
6,925.369 km
Eccentricity
0.00031
Inclination
97.4805°
RAAN
309.2246°
Arg. of periapsis
257.7198°
True anomaly
102.40291°
Mean anomaly
102.3679°
Eccentric anomaly
102.38541°
Mean motion
3.76599 °/min
Orbital period
95.59 mins
BSTAR
0.000064926
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Other satellites on launch #9 in the year 2025 (2025-01-14 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-014 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 | 2026-08-26 17:29:04.564Z | 19.273° NNE | 2026-08-26 17:33:04.564Z | 130.673° SE | 40.796° | 2026-08-26 17:36:04.564Z | 181.157° SSW |
| 5 mins | 2026-08-27 04:15:04.564Z | 112.554° SE | 2026-08-27 04:17:04.564Z | 59.902° ENE | 26.466° | 2026-08-27 04:20:04.564Z | 10.146° NNE |
| 4 mins | 2026-08-27 05:50:04.564Z | 239.978° WSW | 2026-08-27 05:51:04.564Z | 258.211° W | 17.015° | 2026-08-27 05:54:04.564Z | 309.072° 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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