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, 0.2 m
Radar Cross Section
0.240 m², Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 9 hours ago
TLE from 9 hours ago
0 ION SCV-012
1 60573U 24149DK 26219.77351527 .00000338 00000-0 36051-4 0 9991
2 60573 97.6750 292.7033 0001712 270.6664 89.4360 14.95033198107624Epoch: 2026-08-07T18:33Z
TLE epoch observation values (Epoch: 2026-08-07T18:33:51.719Z)
Latitude
-0.00007°
Longitude
57.94342°
Altitude
585.307 km
Speed
7.568 km/s
True Right ascension
19h 30m 48s
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
17:39:33
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
580.472 km
Perigee altitude
578.089 km
Semi-major axis
6,957.418 km
Eccentricity
0.00017
Inclination
97.675°
RAAN
292.7033°
Arg. of periapsis
270.6664°
True anomaly
89.45562°
Mean anomaly
89.436°
Eccentric anomaly
89.44581°
Mean motion
3.74 °/min
Orbital period
96.26 mins
BSTAR
0.000036051
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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 | 2026-08-08 04:20:22.405Z | 130.308° SE | 2026-08-08 04:23:22.405Z | 72.699° E | 28.302° | 2026-08-08 04:26:22.405Z | 12.905° NNE |
| 4 mins | 2026-08-08 05:57:22.405Z | 239.609° WSW | 2026-08-08 05:58:22.405Z | 257.163° W | 17.306° | 2026-08-08 06:01:22.405Z | 307.353° NW |
| 6 mins | 2026-08-08 17:38:22.405Z | 24.617° NE | 2026-08-08 17:40:22.405Z | 75.173° E | 41.825° | 2026-08-08 17:44:22.405Z | 183.171° SSW |
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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