ION SCV-020, 64545
Orbit data source: Space-Track
ION SCV-020, 64545 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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64545 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, Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 1 day ago
TLE from 1 day ago
0 ION SCV-020
1 64545U 25135T 26071.27746575 .00005034 00000-0 23365-3 0 9993
2 64545 97.4577 187.2365 0002992 134.0678 226.0804 15.20479052 40122Epoch: 2026-03-12T06:39Z
TLE epoch observation values (Epoch: 2026-03-12T06:39:33.040Z)
Latitude
-0.00004°
Longitude
-82.58082°
Altitude
508.913 km
Speed
7.609 km/s
True Right ascension
12h 28m 56s
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
11:57:16
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
503.42 km
Perigee altitude
499.304 km
Semi-major axis
6,879.499 km
Eccentricity
0.0003
Inclination
97.4577°
RAAN
187.2365°
Arg. of periapsis
134.0678°
True anomaly
226.05571°
Mean anomaly
226.0804°
Eccentric anomaly
226.06805°
Mean motion
3.80371 °/min
Orbital period
94.64 mins
BSTAR
0.00023365
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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-020 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 | 2026-03-13 08:02:55.969Z | 188.222° SSW | 2026-03-13 08:05:55.969Z | 246.554° WSW | 34.677° | 2026-03-13 08:08:55.969Z | 330.073° NNW |
| 4 mins | 2026-03-13 21:08:55.969Z | 324.829° NNW | 2026-03-13 21:09:55.969Z | 297.448° NW | 26.252° | 2026-03-13 21:12:55.969Z | 230.619° WSW |
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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