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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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: 2 days ago
TLE from 2 days ago
0 RROCI-2
1 59106U 24043J 26171.32173205 .00002542 00000-0 20946-3 0 9991
2 59106 97.8496 304.1017 0010748 17.8620 342.2978 14.99950645125236Epoch: 2026-06-20T07:43Z
TLE epoch observation values (Epoch: 2026-06-20T07:43:17.649Z)
Latitude
-0.00007°
Longitude
-80.25985°
Altitude
562.987 km
Speed
7.584 km/s
True Right ascension
20h 16m 24s
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
21:51:19
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
571.522 km
Perigee altitude
556.599 km
Semi-major axis
6,942.198 km
Eccentricity
0.00107
Inclination
97.8496°
RAAN
304.1017°
Arg. of periapsis
17.862°
True anomaly
342.2603°
Mean anomaly
342.2978°
Eccentric anomaly
342.27906°
Mean motion
3.7523 °/min
Orbital period
95.94 mins
BSTAR
0.00020946
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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. |
|---|---|---|---|---|---|---|---|
| 6 mins | 2026-06-22 21:08:15.221Z | 39.488° NE | 2026-06-22 21:11:15.221Z | 98.711° ESE | 26.862° | 2026-06-22 21:14:15.221Z | 155.654° SSE |
| 4 mins | 2026-06-22 22:44:15.221Z | 325.225° NNW | 2026-06-22 22:46:15.221Z | 287.823° WNW | 18.656° | 2026-06-22 22:48:15.221Z | 253.508° W |
| 4 mins | 2026-06-23 07:56:15.221Z | 94.67° ESE | 2026-06-23 07:57:15.221Z | 76.782° E | 17.216° | 2026-06-23 08:00:15.221Z | 25.749° NE |
| 5 mins | 2026-06-23 09:30:15.221Z | 210.311° SW | 2026-06-23 09:32:15.221Z | 253.455° W | 27.508° | 2026-06-23 09:35:15.221Z | 319.57° 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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