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, 0.3 m
Radar Cross Section
0.240 m², Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 5 hours ago
TLE from 5 hours ago
0 ION SCV-020
1 64545U 25135T 26260.29636193 .00002389 00000-0 11512-3 0 9990
2 64545 97.4685 14.1752 0007646 179.6267 180.4975 15.19688820 68833Epoch: 2026-09-17T07:06Z
TLE epoch observation values (Epoch: 2026-09-17T07:06:45.670Z)
Latitude
-0.00003°
Longitude
-88.75072°
Altitude
515.134 km
Speed
7.603 km/s
True Right ascension
00h 56m 42s
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
05:12:20
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
509.011 km
Perigee altitude
498.487 km
Semi-major axis
6,881.886 km
Eccentricity
0.00076
Inclination
97.4685°
RAAN
14.1752°
Arg. of periapsis
179.6267°
True anomaly
180.49674°
Mean anomaly
180.4975°
Eccentric anomaly
180.49712°
Mean motion
3.80174 °/min
Orbital period
94.69 mins
BSTAR
0.00011512
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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 | 2026-09-17 20:18:59.465Z | 22.392° NNE | 2026-09-17 20:21:59.465Z | 81.956° E | 54.06° | 2026-09-17 20:24:59.465Z | 175.605° S |
| 4 mins | 2026-09-18 06:58:59.465Z | 98.925° ESE | 2026-09-18 06:59:59.465Z | 76.539° E | 22.355° | 2026-09-18 07:02:59.465Z | 19.635° NNE |
| 4 mins | 2026-09-18 08:32:59.465Z | 240.484° WSW | 2026-09-18 08:33:59.465Z | 263.617° W | 21.948° | 2026-09-18 08:36:59.465Z | 317.213° NNW |
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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