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: 14 hours ago
TLE from 14 hours ago
0 ION SCV-014
1 62630U 25009X 26080.48669490 .00002433 00000-0 17594-3 0 9996
2 62630 97.4911 156.2824 0006176 82.9373 277.2555 15.04933781 64790Epoch: 2026-03-21T11:40Z
TLE epoch observation values (Epoch: 2026-03-21T11:40:50.439Z)
Latitude
-0.0001°
Longitude
162.06554°
Altitude
554.238 km
Speed
7.585 km/s
True Right ascension
10h 25m 07s
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
06:45:29
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
552.977 km
Perigee altitude
544.421 km
Semi-major axis
6,926.836 km
Eccentricity
0.00062
Inclination
97.4911°
RAAN
156.2824°
Arg. of periapsis
82.9373°
True anomaly
277.18529°
Mean anomaly
277.2555°
Eccentric anomaly
277.22039°
Mean motion
3.76479 °/min
Orbital period
95.62 mins
BSTAR
0.00017594
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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. |
|---|---|---|---|---|---|---|---|
| 5 mins | 2026-03-22 05:22:36.826Z | 197.982° SSW | 2026-03-22 05:24:36.826Z | 265.345° W | 37.006° | 2026-03-22 05:27:36.826Z | 333.151° NNW |
| 4 mins | 2026-03-22 17:00:36.826Z | 71.278° E | 2026-03-22 17:01:36.826Z | 91.673° ESE | 18.866° | 2026-03-22 17:04:36.826Z | 142.277° SSE |
| 5 mins | 2026-03-22 18:34:36.826Z | 331.936° NNW | 2026-03-22 18:36:36.826Z | 286.035° WNW | 24.619° | 2026-03-22 18:39:36.826Z | 232.639° WSW |
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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