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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Edit Public Description
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: 7 hours ago
TLE from 7 hours ago
0 ION SCV-016
1 62628U 25009V 25290.92227291 .00041947 00000-0 94345-3 0 9995
2 62628 97.4728 351.7147 0619254 144.7291 219.6569 14.43142764 40532Epoch: 2025-10-17T22:08Z
TLE epoch observation values (Epoch: 2025-10-17T22:08:04.379Z)
Latitude
-0.00001°
Longitude
-6.96424°
Altitude
1,101.335 km
Speed
7.12 km/s
True Right ascension
23h 26m 51s
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
00:17:37
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,186.303 km
Perigee altitude
304.074 km
Semi-major axis
7,123.326 km
Eccentricity
0.06193
Inclination
97.4728°
RAAN
351.7147°
Arg. of periapsis
144.7291°
True anomaly
215.38738°
Mean anomaly
219.6569°
Eccentric anomaly
217.49712°
Mean motion
3.6101 °/min
Orbital period
99.72 mins
BSTAR
0.00094345
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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. |
|---|---|---|---|---|---|---|---|
| 4 mins | 2025-10-18 17:02:14.642Z | 14.289° NNE | 2025-10-18 17:04:14.642Z | 179.165° S | 41.766° | 2025-10-18 17:06:14.642Z | 190.707° SSW |
| 9 mins | 2025-10-19 04:12:14.642Z | 168.061° S | 2025-10-19 04:17:14.642Z | 317.704° NNW | 44.793° | 2025-10-19 04:21:14.642Z | 346.922° N |
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 ascending 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 ascending order |
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