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, 2.0 m
Radar Cross Section
0.240 m², Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 11 hours ago
TLE from 11 hours ago
0 ION SCV-016
1 62628U 25009V 26305.01416547 .00023596 00000-0 47833-3 0 9997
2 62628 97.4163 328.4381 0569203 32.4538 331.0359 14.55923819 95426Epoch: 2026-11-01T00:20Z
TLE epoch observation values (Epoch: 2026-11-01T00:20:23.896Z)
Latitude
0.00002°
Longitude
-76.97309°
Altitude
362.294 km
Speed
7.878 km/s
True Right ascension
21h 53m 45s
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
07:21:22
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,106.488 km
Perigee altitude
300.321 km
Semi-major axis
7,081.541 km
Eccentricity
0.05692
Inclination
97.4163°
RAAN
328.4381°
Arg. of periapsis
32.4538°
True anomaly
327.67014°
Mean anomaly
331.0359°
Eccentric anomaly
329.37452°
Mean motion
3.6421 °/min
Orbital period
98.84 mins
BSTAR
0.00047833
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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. |
|---|---|---|---|---|---|---|---|
| 10 mins | 2026-11-01 14:03:44.338Z | 26.303° NE | 2026-11-01 14:07:44.338Z | 83.181° E | 47.05° | 2026-11-01 14:13:44.338Z | 173.367° S |
| 6 mins | 2026-11-01 15:43:44.338Z | 323.126° NNW | 2026-11-01 15:45:44.338Z | 292.842° NW | 21.794° | 2026-11-01 15:49:44.338Z | 244.692° WSW |
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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Click to sort rows by Secondary header in ascending order | Click to sort rows by Secondary name header in ascending order | Click to sort rows by Country header in ascending order | Click to sort rows by Owner header in ascending order | Click to sort rows by Obj. Type header in ascending order | Click to sort rows by Miss dist. header in ascending order | Click to sort rows by Rel. speed header in ascending order | Click to sort rows by Apr. angle header in ascending order | Click to sort rows by TCA header in descending order |
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