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: 11 hours ago
TLE from 11 hours ago
0 RROCI-2
1 59106U 24043J 25289.09768272 .00005497 00000-0 46839-3 0 9999
2 59106 97.8158 55.6996 0009332 94.1580 266.0709 14.98144278 88199Epoch: 2025-10-16T02:20Z
TLE epoch observation values (Epoch: 2025-10-16T02:20:39.787Z)
Latitude
0.00003°
Longitude
-4.32847°
Altitude
576.13 km
Speed
7.572 km/s
True Right ascension
03h 42m 47s
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
08:27:44
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
576.127 km
Perigee altitude
563.159 km
Semi-major axis
6,947.78 km
Eccentricity
0.00093
Inclination
97.8158°
RAAN
55.6996°
Arg. of periapsis
94.158°
True anomaly
265.96422°
Mean anomaly
266.0709°
Eccentric anomaly
266.01756°
Mean motion
3.74778 °/min
Orbital period
96.06 mins
BSTAR
0.00046839
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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 | 2025-10-16 20:33:52.707Z | 52.637° ENE | 2025-10-16 20:35:52.707Z | 86.285° E | 18.855° | 2025-10-16 20:38:52.707Z | 139.03° SSE |
| 5 mins | 2025-10-16 22:09:52.707Z | 327.185° NNW | 2025-10-16 22:11:52.707Z | 277.243° WNW | 25.055° | 2025-10-16 22:14:52.707Z | 230.118° WSW |
| 6 mins | 2025-10-17 08:55:52.707Z | 190.965° SSW | 2025-10-17 08:58:52.707Z | 276.139° WNW | 36.481° | 2025-10-17 09:01:52.707Z | 333.343° 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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