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: 13 hours ago
TLE from 13 hours ago
0 ION SCV-012
1 60573U 24149DK 25289.20687656 .00001839 00000-0 17712-3 0 9999
2 60573 97.7050 3.1313 0003783 154.8447 205.2958 14.94150564 63476Epoch: 2025-10-16T04:57Z
TLE epoch observation values (Epoch: 2025-10-16T04:57:54.134Z)
Latitude
-0.00006°
Longitude
-96.31417°
Altitude
590.439 km
Speed
7.564 km/s
True Right ascension
00h 12m 31s
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
12:32:39
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
584.657 km
Perigee altitude
579.391 km
Semi-major axis
6,960.161 km
Eccentricity
0.00038
Inclination
97.705°
RAAN
3.1313°
Arg. of periapsis
154.8447°
True anomaly
205.27728°
Mean anomaly
205.2958°
Eccentric anomaly
205.28654°
Mean motion
3.73778 °/min
Orbital period
96.31 mins
BSTAR
0.00017712
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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. |
|---|---|---|---|---|---|---|---|
| 7 mins | 2025-10-16 18:23:08.218Z | 354.511° N | 2025-10-16 18:26:08.218Z | 298.021° NW | 33.374° | 2025-10-16 18:30:08.218Z | 217.364° SW |
| 7 mins | 2025-10-17 05:12:08.218Z | 175.41° S | 2025-10-17 05:15:08.218Z | 259.315° W | 43.656° | 2025-10-17 05:19:08.218Z | 343.455° N |
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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