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, 0.3 m
Radar Cross Section
0.240 m², Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 6 hours ago
TLE from 6 hours ago
0 ION SCV-014
1 62630U 25009X 26307.62970044 .00000700 00000-0 52738-4 0 9999
2 62630 97.4716 16.5235 0005560 39.0156 321.1472 15.05571425 98962Epoch: 2026-11-03T15:06Z
TLE epoch observation values (Epoch: 2026-11-03T15:06:46.118Z)
Latitude
0.00008°
Longitude
106.94171°
Altitude
549.821 km
Speed
7.589 km/s
True Right ascension
01h 06m 05s
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
17:14:42
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
550.59 km
Perigee altitude
542.89 km
Semi-major axis
6,924.877 km
Eccentricity
0.00056
Inclination
97.4716°
RAAN
16.5235°
Arg. of periapsis
39.0156°
True anomaly
321.10721°
Mean anomaly
321.1472°
Eccentric anomaly
321.12721°
Mean motion
3.76639 °/min
Orbital period
95.58 mins
BSTAR
0.000052738
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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. |
|---|---|---|---|---|---|---|---|
| 6 mins | 2026-11-04 04:00:35.162Z | 124.226° SE | 2026-11-04 04:03:35.162Z | 73.395° E | 24.449° | 2026-11-04 04:06:35.162Z | 18.187° NNE |
| 4 mins | 2026-11-04 05:36:35.162Z | 228.188° WSW | 2026-11-04 05:38:35.162Z | 269.716° W | 22.374° | 2026-11-04 05:40:35.162Z | 307.586° NW |
| 6 mins | 2026-11-04 17:12:35.162Z | 31.919° NE | 2026-11-04 17:15:35.162Z | 108.358° ESE | 42.813° | 2026-11-04 17:18:35.162Z | 168.409° S |
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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