ION SCV-012, 60573
Orbit data source: Space-Track
ION SCV-012, 60573 is a payload satellite owned by D-ORBIT (IT) in SSO that was launched on Fri, 16 Aug 2024 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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60573 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: 10 hours ago
TLE from 10 hours ago
0 ION SCV-012
1 60573U 24149DK 26265.08397881 .00001034 00000-0 99494-4 0 9993
2 60573 97.6698 337.0315 0004741 110.9645 249.2084 14.95099354114398Epoch: 2026-09-22T02:00Z
TLE epoch observation values (Epoch: 2026-09-22T02:00:55.769Z)
Latitude
0.00005°
Longitude
-54.15542°
Altitude
586.286 km
Speed
7.566 km/s
True Right ascension
22h 28m 07s
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
05:26:56
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
582.373 km
Perigee altitude
575.776 km
Semi-major axis
6,957.212 km
Eccentricity
0.00047
Inclination
97.6698°
RAAN
337.0315°
Arg. of periapsis
110.9645°
True anomaly
249.15762°
Mean anomaly
249.2084°
Eccentric anomaly
249.18301°
Mean motion
3.74016 °/min
Orbital period
96.25 mins
BSTAR
0.000099494
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Other satellites on launch #149 in the year 2024 (2024-08-16 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-012 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 | 2026-09-22 17:02:53.643Z | 40.694° NE | 2026-09-22 17:05:53.643Z | 92.437° ESE | 26.277° | 2026-09-22 17:08:53.643Z | 148.477° SSE |
| 4 mins | 2026-09-22 18:39:53.643Z | 320.006° NNW | 2026-09-22 18:40:53.643Z | 299.663° NW | 22.922° | 2026-09-22 18:43:53.643Z | 244.566° WSW |
| 5 mins | 2026-09-23 05:27:53.643Z | 211.454° SW | 2026-09-23 05:29:53.643Z | 267.186° W | 37.614° | 2026-09-23 05:32:53.643Z | 326.472° 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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