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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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, Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 10 hours ago
TLE from 10 hours ago
0 ION SCV-020
1 64545U 25135T 25328.29944670 .00004275 00000-0 20710-3 0 9992
2 64545 97.4574 80.5280 0002537 128.1213 232.0250 15.19071777 23723Epoch: 2025-11-24T07:11Z
TLE epoch observation values (Epoch: 2025-11-24T07:11:12.194Z)
Latitude
-0.0001°
Longitude
-90.7742°
Altitude
512.808 km
Speed
7.607 km/s
True Right ascension
05h 22m 06s
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
14:02:52
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
507.36 km
Perigee altitude
503.867 km
Semi-major axis
6,883.751 km
Eccentricity
0.00025
Inclination
97.4574°
RAAN
80.528°
Arg. of periapsis
128.1213°
True anomaly
232.00209°
Mean anomaly
232.025°
Eccentric anomaly
232.01354°
Mean motion
3.80019 °/min
Orbital period
94.73 mins
BSTAR
0.0002071
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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 | 2025-11-24 20:23:45.912Z | 17.024° NNE | 2025-11-24 20:26:45.912Z | 83.023° E | 43.586° | 2025-11-24 20:29:45.912Z | 185.36° SSW |
| 4 mins | 2025-11-25 07:03:45.912Z | 107.692° ESE | 2025-11-25 07:04:45.912Z | 82.716° E | 24.651° | 2025-11-25 07:07:45.912Z | 16.734° NNE |
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 ascending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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