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, 0.3 m
Radar Cross Section
0.240 m², Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 1 day ago
TLE from 1 day ago
0 ION SCV-018
1 64575U 25135AZ 26259.26451777 .00001045 00000-0 10133-3 0 9997
2 64575 97.7857 13.5787 0012302 356.1385 3.9739 14.94784942 67536Epoch: 2026-09-16T06:20Z
TLE epoch observation values (Epoch: 2026-09-16T06:20:54.335Z)
Latitude
0.00005°
Longitude
-76.8663°
Altitude
577.541 km
Speed
7.576 km/s
True Right ascension
00h 54m 18s
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
07:19:09
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
588.616 km
Perigee altitude
571.496 km
Semi-major axis
6,958.193 km
Eccentricity
0.00123
Inclination
97.7857°
RAAN
13.5787°
Arg. of periapsis
356.1385°
True anomaly
3.98368°
Mean anomaly
3.9739°
Eccentric anomaly
3.97879°
Mean motion
3.73937 °/min
Orbital period
96.27 mins
BSTAR
0.00010133
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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 | 2026-09-17 19:52:28.165Z | 39.831° NE | 2026-09-17 19:55:28.165Z | 89.602° E | 26.682° | 2026-09-17 19:58:28.165Z | 147.419° SSE |
| 4 mins | 2026-09-17 21:29:28.165Z | 322.163° NNW | 2026-09-17 21:30:28.165Z | 302.485° NW | 23.075° | 2026-09-17 21:33:28.165Z | 246.22° WSW |
| 5 mins | 2026-09-18 08:17:28.165Z | 208.946° SW | 2026-09-18 08:19:28.165Z | 258.743° W | 36.557° | 2026-09-18 08:22:28.165Z | 323.894° 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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