RROCI-2, 59106
Orbit data source: Space-Track
RROCI-2, 59106 is an American payload satellite in SSO that was launched on Mon, 04 Mar 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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59106 intel report (Beta)
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Edit Public Description
Identifier
Orbit
Country
USRelated business
Manufacturer
Orion Space Sol.
Mission
Operational Commercial Weather
Bus & Motor
CUBESAT 12U, Unknown motor
Mass
19 kg wet, 19 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Box + 2 Pan, 0.5 m
Radar Cross Section
0.126 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 10 hours ago
TLE from 10 hours ago
0 RROCI-2
1 59106U 24043J 25341.91995975 .00004834 00000-0 40725-3 0 9993
2 59106 97.8247 108.6482 0005827 279.8506 80.2059 14.98664090 96105Epoch: 2025-12-07T22:04Z
TLE epoch observation values (Epoch: 2025-12-07T22:04:44.522Z)
Latitude
0.00005°
Longitude
60.53625°
Altitude
573.385 km
Speed
7.574 km/s
True Right ascension
07h 14m 35s
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
05:47:13
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
572.083 km
Perigee altitude
563.988 km
Semi-major axis
6,946.173 km
Eccentricity
0.00058
Inclination
97.8247°
RAAN
108.6482°
Arg. of periapsis
279.8506°
True anomaly
80.27171°
Mean anomaly
80.2059°
Eccentric anomaly
80.2388°
Mean motion
3.74908 °/min
Orbital period
96.02 mins
BSTAR
0.00040725
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Other satellites on launch #43 in the year 2024 (2024-03-04 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.RROCI-2 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. |
|---|---|---|---|---|---|---|---|
| 5 mins | 2025-12-08 07:50:25.015Z | 117.758° SE | 2025-12-08 07:53:25.015Z | 60.968° ENE | 22.259° | 2025-12-08 07:55:25.015Z | 24.272° NE |
| 5 mins | 2025-12-08 09:26:25.015Z | 228.438° WSW | 2025-12-08 09:28:25.015Z | 271.645° WNW | 22.171° | 2025-12-08 09:31:25.015Z | 319.531° NNW |
| 5 mins | 2025-12-08 21:06:25.015Z | 42.73° NE | 2025-12-08 21:08:25.015Z | 103.803° ESE | 34.327° | 2025-12-08 21:11:25.015Z | 167.379° S |
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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