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: 17 hours ago
TLE from 17 hours ago
0 ION SCV-020
1 64545U 25135T 25269.26578183 .00007803 00000-0 38302-3 0 9991
2 64545 97.4523 22.3068 0001876 49.7697 310.3701 15.18357296 14761Epoch: 2025-09-26T06:22Z
TLE epoch observation values (Epoch: 2025-09-26T06:22:43.550Z)
Latitude
-0°
Longitude
-78.68969°
Altitude
513.055 km
Speed
7.608 km/s
True Right ascension
01h 29m 13s
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
17:08:17
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
509.067 km
Perigee altitude
506.483 km
Semi-major axis
6,885.912 km
Eccentricity
0.00019
Inclination
97.4523°
RAAN
22.3068°
Arg. of periapsis
49.7697°
True anomaly
310.35372°
Mean anomaly
310.3701°
Eccentric anomaly
310.36191°
Mean motion
3.7984 °/min
Orbital period
94.78 mins
BSTAR
0.00038302
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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 | 2025-09-27 07:48:39.332Z | 176.054° S | 2025-09-27 07:51:39.332Z | 263.432° W | 43.149° | 2025-09-27 07:54:39.332Z | 341.699° N |
| 5 mins | 2025-09-27 20:54:39.332Z | 347.986° N | 2025-09-27 20:56:39.332Z | 292.828° NW | 34.235° | 2025-09-27 20:59:39.332Z | 218.113° SW |
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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Click to sort rows by Secondary header in ascending order | Click to sort rows by Secondary name header in ascending order | Click to sort rows by Country header in ascending order | Click to sort rows by Owner header in ascending order | Click to sort rows by Obj. Type header in ascending order | Click to sort rows by Miss dist. header in ascending order | Click to sort rows by Rel. speed header in ascending order | Click to sort rows by Apr. angle header in ascending order | Click to sort rows by TCA header in ascending order |
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