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 26083.32829194 .00001624 00000-0 15570-3 0 9994
2 64575 97.7662 199.2303 0012004 209.4115 150.6431 14.94471888 41258Epoch: 2026-03-24T07:52Z
TLE epoch observation values (Epoch: 2026-03-24T07:52:44.423Z)
Latitude
-0.00003°
Longitude
-100.76231°
Altitude
594.346 km
Speed
7.559 km/s
True Right ascension
13h 16m 55s
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
00:47:55
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
589.382 km
Perigee altitude
572.674 km
Semi-major axis
6,959.165 km
Eccentricity
0.0012
Inclination
97.7662°
RAAN
199.2303°
Arg. of periapsis
209.4115°
True anomaly
150.71045°
Mean anomaly
150.6431°
Eccentric anomaly
150.67678°
Mean motion
3.73859 °/min
Orbital period
96.29 mins
BSTAR
0.0001557
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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. |
|---|---|---|---|---|---|---|---|
| 5 mins | 2026-03-24 19:43:14.229Z | 53.496° ENE | 2026-03-24 19:45:14.229Z | 89.763° E | 20.733° | 2026-03-24 19:48:14.229Z | 142.817° SSE |
| 5 mins | 2026-03-24 21:19:14.229Z | 326.156° NNW | 2026-03-24 21:21:14.229Z | 279.524° WNW | 23.953° | 2026-03-24 21:24:14.229Z | 232.814° WSW |
| 6 mins | 2026-03-25 08:07:14.229Z | 199.996° SSW | 2026-03-25 08:09:14.229Z | 248.866° W | 34.445° | 2026-03-25 08:13:14.229Z | 332.887° 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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