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: 12 hours ago
TLE from 12 hours ago
0 ION SCV-018
1 64575U 25135AZ 26133.07349510 .00000785 00000-0 77745-4 0 9991
2 64575 97.7736 248.4764 0013783 54.1428 306.1070 14.94587236 48681Epoch: 2026-05-13T01:45Z
TLE epoch observation values (Epoch: 2026-05-13T01:45:49.976Z)
Latitude
-0.00005°
Longitude
-8.82058°
Altitude
581.052 km
Speed
7.573 km/s
True Right ascension
16h 33m 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
22:06:32
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
590.261 km
Perigee altitude
571.079 km
Semi-major axis
6,958.807 km
Eccentricity
0.00138
Inclination
97.7736°
RAAN
248.4764°
Arg. of periapsis
54.1428°
True anomaly
305.97927°
Mean anomaly
306.107°
Eccentric anomaly
306.04315°
Mean motion
3.73888 °/min
Orbital period
96.29 mins
BSTAR
0.000077745
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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 | 2026-05-13 20:00:42.179Z | 34.598° NE | 2026-05-13 20:03:42.179Z | 90.773° ESE | 29.812° | 2026-05-13 20:06:42.179Z | 157.415° SSE |
| 4 mins | 2026-05-13 21:37:42.179Z | 316.851° NNW | 2026-05-13 21:38:42.179Z | 299.222° NW | 16.944° | 2026-05-13 21:41:42.179Z | 251.376° W |
| 5 mins | 2026-05-14 06:50:42.179Z | 106.662° ESE | 2026-05-14 06:52:42.179Z | 68.525° E | 20.639° | 2026-05-14 06:55:42.179Z | 18.806° NNE |
| 5 mins | 2026-05-14 08:25:42.179Z | 217.273° SW | 2026-05-14 08:27:42.179Z | 257.256° W | 24.217° | 2026-05-14 08:30:42.179Z | 316.206° NNW |
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 descending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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