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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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, Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 20 hours ago
TLE from 20 hours ago
0 ION SCV-012
1 60573U 24149DK 25338.55954299 .00003544 00000-0 33456-3 0 9990
2 60573 97.7009 51.5405 0003957 36.3069 323.8419 14.94367140 70844Epoch: 2025-12-04T13:25Z
TLE epoch observation values (Epoch: 2025-12-04T13:25:44.514Z)
Latitude
-0.00003°
Longitude
136.49079°
Altitude
585.16 km
Speed
7.569 km/s
True Right ascension
03h 26m 09s
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
07:18:05
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
584.104 km
Perigee altitude
578.597 km
Semi-major axis
6,959.488 km
Eccentricity
0.0004
Inclination
97.7009°
RAAN
51.5405°
Arg. of periapsis
36.3069°
True anomaly
323.81514°
Mean anomaly
323.8419°
Eccentric anomaly
323.82852°
Mean motion
3.73833 °/min
Orbital period
96.3 mins
BSTAR
0.00033456
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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 | 2025-12-05 17:19:50.183Z | 39.841° NE | 2025-12-05 17:22:50.183Z | 105.548° ESE | 28.547° | 2025-12-05 17:25:50.183Z | 159.323° S |
| 4 mins | 2025-12-06 04:09:50.183Z | 99.34° ESE | 2025-12-06 04:11:50.183Z | 60.088° ENE | 19.548° | 2025-12-06 04:13:50.183Z | 26.49° NE |
| 5 mins | 2025-12-06 05:44:50.183Z | 220.903° SW | 2025-12-06 05:46:50.183Z | 267.651° W | 25.875° | 2025-12-06 05:49:50.183Z | 321.307° 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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