ION SCV-018, 64575
Orbit data source: Space-Track
ION SCV-018, 64575 is a payload satellite owned by D-ORBIT (IT) in SSO that was launched on Mon, 23 Jun 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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64575 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, 0.2 m
Radar Cross Section
0.240 m², Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 9 hours ago
TLE from 9 hours ago
0 ION SCV-018
1 64575U 25135AZ 25328.32991113 .00001852 00000-0 17870-3 0 9994
2 64575 97.7630 80.5720 0011393 252.7881 107.2092 14.94059124 23334Epoch: 2025-11-24T07:55Z
TLE epoch observation values (Epoch: 2025-11-24T07:55:04.321Z)
Latitude
-0.00005°
Longitude
-101.72743°
Altitude
590.695 km
Speed
7.563 km/s
True Right ascension
05h 22m 17s
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
13:56:54
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
590.241 km
Perigee altitude
574.381 km
Semi-major axis
6,960.448 km
Eccentricity
0.00114
Inclination
97.763°
RAAN
80.572°
Arg. of periapsis
252.7881°
True anomaly
107.33386°
Mean anomaly
107.2092°
Eccentric anomaly
107.27153°
Mean motion
3.73755 °/min
Orbital period
96.32 mins
BSTAR
0.0001787
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Other satellites on launch #135 in the year 2025 (2025-06-23 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-018 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 | 2025-11-24 19:44:48.718Z | 41.439° NE | 2025-11-24 19:47:48.718Z | 91.208° ESE | 22.881° | 2025-11-24 19:50:48.718Z | 146.316° SSE |
| 4 mins | 2025-11-24 21:21:48.718Z | 323.152° NNW | 2025-11-24 21:23:48.718Z | 279.201° WNW | 22.2° | 2025-11-24 21:25:48.718Z | 244.582° WSW |
| 6 mins | 2025-11-25 08:09:48.718Z | 203.243° SW | 2025-11-25 08:11:48.718Z | 247.012° WSW | 31.712° | 2025-11-25 08:15:48.718Z | 330.026° NNW |
Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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