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, 1.9 m
Radar Cross Section
0.240 m², Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 18 hours ago
TLE from 18 hours ago
0 ION SCV-014
1 62630U 25009X 26171.10280226 .00000945 00000-0 70373-4 0 9993
2 62630 97.4852 244.1797 0006026 121.6757 238.5058 15.05233877 78424Epoch: 2026-06-20T02:28Z
TLE epoch observation values (Epoch: 2026-06-20T02:28:02.115Z)
Latitude
-0.00003°
Longitude
-61.15135°
Altitude
556.039 km
Speed
7.582 km/s
True Right ascension
16h 16m 43s
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
07:22:45
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
551.95 km
Perigee altitude
543.603 km
Semi-major axis
6,925.914 km
Eccentricity
0.0006
Inclination
97.4852°
RAAN
244.1797°
Arg. of periapsis
121.6757°
True anomaly
238.44694°
Mean anomaly
238.5058°
Eccentric anomaly
238.47637°
Mean motion
3.76554 °/min
Orbital period
95.6 mins
BSTAR
0.000070373
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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 | 2026-06-21 04:07:58.964Z | 122.436° SE | 2026-06-21 04:10:58.964Z | 71.021° E | 21.84° | 2026-06-21 04:13:58.964Z | 17.93° NNE |
| 4 mins | 2026-06-21 05:43:58.964Z | 228.4° WSW | 2026-06-21 05:45:58.964Z | 271.559° WNW | 21.438° | 2026-06-21 05:47:58.964Z | 309.264° NW |
| 5 mins | 2026-06-21 17:20:58.964Z | 43.971° NE | 2026-06-21 17:22:58.964Z | 106.593° ESE | 33.076° | 2026-06-21 17:25:58.964Z | 166.872° 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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