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, 0.3 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 26256.05029396 .00018548 00000-0 38576-3 0 9993
2 62628 97.4224 284.6729 0575227 187.7047 171.5026 14.54163107 88307Epoch: 2026-09-13T01:12Z
TLE epoch observation values (Epoch: 2026-09-13T01:12:25.398Z)
Latitude
0.00001°
Longitude
-85.48344°
Altitude
1,119.021 km
Speed
7.082 km/s
True Right ascension
18h 58m 41s
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
04:21:20
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,116.802 km
Perigee altitude
301.446 km
Semi-major axis
7,087.261 km
Eccentricity
0.05752
Inclination
97.4224°
RAAN
284.6729°
Arg. of periapsis
187.7047°
True anomaly
172.41175°
Mean anomaly
171.5026°
Eccentric anomaly
171.96337°
Mean motion
3.63769 °/min
Orbital period
98.96 mins
BSTAR
0.00038576
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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. |
|---|---|---|---|---|---|---|---|
| 5 mins | 2026-09-13 15:01:52.145Z | 5.282° NNE | 2026-09-13 15:04:52.145Z | 295.416° NW | 63.241° | 2026-09-13 15:06:52.145Z | 207.057° SW |
| 6 mins | 2026-09-14 00:30:52.145Z | 93.042° ESE | 2026-09-14 00:33:52.145Z | 61.554° ENE | 18.06° | 2026-09-14 00:36:52.145Z | 29.802° NE |
| 11 mins | 2026-09-14 02:05:52.145Z | 170.464° S | 2026-09-14 02:10:52.145Z | 231.145° WSW | 81.96° | 2026-09-14 02:16:52.145Z | 346.231° N |
| 4 mins | 2026-09-14 03:47:52.145Z | 256.284° W | 2026-09-14 03:49:52.145Z | 275.442° WNW | 13.315° | 2026-09-14 03:51:52.145Z | 294.401° 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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