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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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, 1.1 m
Radar Cross Section
0.240 m², Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 19 hours ago
TLE from 19 hours ago
0 ION SCV-014
1 62630U 25009X 25290.19183672 .00002351 00000-0 17411-3 0 9996
2 62630 97.5128 5.4755 0003274 235.3875 124.7043 15.04080155 41449Epoch: 2025-10-17T04:36Z
TLE epoch observation values (Epoch: 2025-10-17T04:36:14.692Z)
Latitude
0°
Longitude
-89.52646°
Altitude
558.689 km
Speed
7.581 km/s
True Right ascension
00h 21m 54s
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
18:33:38
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
553.591 km
Perigee altitude
549.054 km
Semi-major axis
6,929.459 km
Eccentricity
0.00033
Inclination
97.5128°
RAAN
5.4755°
Arg. of periapsis
235.3875°
True anomaly
124.73514°
Mean anomaly
124.7043°
Eccentric anomaly
124.71972°
Mean motion
3.76265 °/min
Orbital period
95.68 mins
BSTAR
0.00017411
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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 | 2025-10-18 04:41:12.062Z | 138.03° SSE | 2025-10-18 04:44:12.062Z | 77.741° E | 31.96° | 2025-10-18 04:47:12.062Z | 9.272° NNE |
| 6 mins | 2025-10-18 17:54:12.062Z | 18.464° NNE | 2025-10-18 17:57:12.062Z | 146.044° SSE | 42.839° | 2025-10-18 18:00:12.062Z | 186.221° SSW |
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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