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: 22 hours ago
TLE from 22 hours ago
0 ION SCV-018
1 64575U 25135AZ 26035.31955288 .00001671 00000-0 16061-3 0 9992
2 64575 97.7632 151.7442 0013039 21.0861 339.0894 14.94328172 34083Epoch: 2026-02-04T07:40Z
TLE epoch observation values (Epoch: 2026-02-04T07:40:09.368Z)
Latitude
-0.00005°
Longitude
-97.78266°
Altitude
579.023 km
Speed
7.576 km/s
True Right ascension
10h 06m 58s
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
07:51:47
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
590.549 km
Perigee altitude
572.4 km
Semi-major axis
6,959.611 km
Eccentricity
0.0013
Inclination
97.7632°
RAAN
151.7442°
Arg. of periapsis
21.0861°
True anomaly
339.03599°
Mean anomaly
339.0894°
Eccentric anomaly
339.0627°
Mean motion
3.73823 °/min
Orbital period
96.3 mins
BSTAR
0.00016061
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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 | 2026-02-05 07:54:39.713Z | 184.364° SSW | 2026-02-05 07:56:39.713Z | 225.645° WSW | 39.738° | 2026-02-05 08:00:39.713Z | 338.958° N |
| 4 mins | 2026-02-05 19:37:39.713Z | 64.973° ENE | 2026-02-05 19:39:39.713Z | 102.619° ESE | 18.445° | 2026-02-05 19:41:39.713Z | 134.995° SE |
| 5 mins | 2026-02-05 21:12:39.713Z | 335.44° NNW | 2026-02-05 21:14:39.713Z | 289.525° WNW | 27.345° | 2026-02-05 21:17:39.713Z | 232.106° WSW |
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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