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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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: 10 hours ago
TLE from 10 hours ago
0 ION SCV-018
1 64575U 25135AZ 26178.33018718 .00001271 00000-0 12244-3 0 9995
2 64575 97.7788 293.3198 0011158 256.9420 103.0555 14.94666347 55441Epoch: 2026-06-27T07:55Z
TLE epoch observation values (Epoch: 2026-06-27T07:55:28.172Z)
Latitude
-0.00001°
Longitude
-100.99347°
Altitude
588.217 km
Speed
7.565 km/s
True Right ascension
19h 33m 16s
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
05:14:10
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
588.189 km
Perigee altitude
572.66 km
Semi-major axis
6,958.561 km
Eccentricity
0.00112
Inclination
97.7788°
RAAN
293.3198°
Arg. of periapsis
256.942°
True anomaly
103.18002°
Mean anomaly
103.0555°
Eccentric anomaly
103.11776°
Mean motion
3.73907 °/min
Orbital period
96.28 mins
BSTAR
0.00012244
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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 | 2026-06-27 19:45:13.601Z | 45.636° ENE | 2026-06-27 19:48:13.601Z | 97.628° ESE | 21.343° | 2026-06-27 19:51:13.601Z | 146.808° SSE |
| 5 mins | 2026-06-27 21:21:13.601Z | 335.215° NNW | 2026-06-27 21:23:13.601Z | 295.929° NW | 24.058° | 2026-06-27 21:26:13.601Z | 239.013° WSW |
| 6 mins | 2026-06-28 08:09:13.601Z | 195.714° SSW | 2026-06-28 08:12:13.601Z | 269.371° W | 34.125° | 2026-06-28 08:15:13.601Z | 329.359° 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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