ION SCV-016, 62628
Orbit data source: Space-Track
ION SCV-016, 62628 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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62628 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, 1.4 m
Radar Cross Section
0.240 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 11 hours ago
TLE from 11 hours ago
0 ION SCV-016
1 62628U 25009V 26126.14336050 .00014738 00000-0 32188-3 0 9997
2 62628 97.4322 168.9041 0594270 238.5154 115.6671 14.49189350 69452Epoch: 2026-05-06T03:26Z
TLE epoch observation values (Epoch: 2026-05-06T03:26:26.347Z)
Latitude
-0.00001°
Longitude
-106.71376°
Altitude
933.849 km
Speed
7.279 km/s
True Right ascension
11h 15m 36s
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
22:16:53
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,147.482 km
Perigee altitude
303.205 km
Semi-major axis
7,103.481 km
Eccentricity
0.05943
Inclination
97.4322°
RAAN
168.9041°
Arg. of periapsis
238.5154°
True anomaly
121.60283°
Mean anomaly
115.6671°
Eccentric anomaly
118.65499°
Mean motion
3.62524 °/min
Orbital period
99.3 mins
BSTAR
0.00032188
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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-016 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. |
|---|---|---|---|---|---|---|---|
| 9 mins | 2026-05-06 15:39:32.928Z | 12.033° NNE | 2026-05-06 15:44:32.928Z | 176.817° S | 44.973° | 2026-05-06 15:48:32.928Z | 192.906° SSW |
| 7 mins | 2026-05-07 01:10:32.928Z | 87.147° E | 2026-05-07 01:13:32.928Z | 58.253° ENE | 16.965° | 2026-05-07 01:17:32.928Z | 22.801° NE |
| 12 mins | 2026-05-07 02:45:32.928Z | 163.157° S | 2026-05-07 02:50:32.928Z | 104.738° ESE | 44.859° | 2026-05-07 02:57:32.928Z | 349.44° N |
| 7 mins | 2026-05-07 04:26:32.928Z | 243.11° WSW | 2026-05-07 04:29:32.928Z | 272.47° WNW | 17.117° | 2026-05-07 04:33:32.928Z | 309.199° NW |
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 descending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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