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, Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 10 hours ago
TLE from 10 hours ago
0 ION SCV-020
1 64545U 25135T 26178.30931889 .00003325 00000-0 16063-3 0 9997
2 64545 97.4618 293.1215 0009306 113.5611 246.6602 15.19301254 56389Epoch: 2026-06-27T07:25Z
TLE epoch observation values (Epoch: 2026-06-27T07:25:25.152Z)
Latitude
0°
Longitude
-93.65862°
Altitude
513.583 km
Speed
7.606 km/s
True Right ascension
19h 32m 29s
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
04:24:30
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
511.326 km
Perigee altitude
498.515 km
Semi-major axis
6,883.057 km
Eccentricity
0.00093
Inclination
97.4618°
RAAN
293.1215°
Arg. of periapsis
113.5611°
True anomaly
246.56233°
Mean anomaly
246.6602°
Eccentric anomaly
246.61126°
Mean motion
3.80077 °/min
Orbital period
94.72 mins
BSTAR
0.00016063
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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 | 2026-06-27 20:37:42.444Z | 8.761° NNE | 2026-06-27 20:40:42.444Z | 310.491° NW | 44.284° | 2026-06-27 20:43:42.444Z | 197.988° SSW |
| 5 mins | 2026-06-28 07:16:42.444Z | 132.568° SE | 2026-06-28 07:18:42.444Z | 84.261° E | 31.298° | 2026-06-28 07:21:42.444Z | 9.111° 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 descending 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 descending order |
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