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RROCI-2

In orbit NORAD 59106 ZQDJ-0650-5501-6285-2771

Falcon 9 Block 5

Carrier rocket

Space Launch Complex 4E

Spaceport

0

Observations all time

Mission information
Spacecraft name
RROCI-2
Status
Active
The satellite is in orbit
The network has not received data from this satellite for a long time
Launch and timeline
Carrier rocket
Falcon 9 Block 5
Spaceport
Space Launch Complex 4E
Launch time
2024-03-04 22:05:00
Separation time
2024-04-04 00:34:17
Satellite appearance
Data for the last 30 days
Orbital parameters of the satellite
Perigee
551.48 km
Apogee
574.28 km
Inclination
97.9°
Period
96.0 min
Semi-major axis
6941.0 km
Velocity
7.58 km/s
Orbital elements
TLE source
Celestrak
TLE updated
2026-10-11 12:56:44 UTC
Two-line elements (TLE)
1 59106U 24043J   26284.11378750  .00002555  00000-0  20816-3 0  9995
2 59106 97.8578 57.9234 0016407 12.5743 347.5886 15.00334303142142
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Orbit history, past year

Mean elements of every TLE set over the past 365 days, plotted against the epoch of the set. Each source is its own line; click it in the legend to hide it. A jump in altitude is a manoeuvre or a bad set; lines drifting apart are a disagreement between sources. “TLE age” is how many hours have passed since the epoch of the source's freshest set, plotted against when the set reached us, on a logarithmic scale. A set the source repeats unchanged does not reset the age.

Prediction divergence

Each TLE set is propagated with SGP4 to the epoch of the next set from the same source and compared with it, plotted against the epoch of the next set; the tooltip shows how many hours ahead the prediction ran. The logarithmic scale shows the size of the divergence and the tooltip its sign: plus along-track means the prediction is ahead of the satellite. This is how well the sets agree, not the true error: the reference is a TLE too, off by about a kilometre. An outlier is a manoeuvre between sets. Sets more than a week apart are not compared.

Time of closest approach, UTC Object 1 Object 2 Distance, km Speed, km/s Max. probability
2026-10-12 05:25:30 RROCI-2
NORAD 59106
STARLINK-36163
NORAD 67008
3.327 14.57 5.0e-06
2026-10-12 12:39:06 RROCI-2
NORAD 59106
CZ-6A DEB
NORAD 60898
4.631 15.04 7.5e-08
2026-10-13 15:42:40 YAOGAN-30 06C
NORAD 44451
RROCI-2
NORAD 59106
2.714 11.48 4.2e-07
2026-10-13 16:39:25 RROCI-2
NORAD 59106
STARLINK-36280
NORAD 67211
3.121 9.67 1.1e-05
2026-10-13 17:38:24 STARLINK-5582
NORAD 56777
RROCI-2
NORAD 59106
4.561 11.32 4.6e-06
2026-10-13 17:50:50 STARLINK-5630
NORAD 55406
RROCI-2
NORAD 59106
3.696 15.04 3.4e-06
2026-10-14 03:49:12 RROCI-2
NORAD 59106
STARLINK-36120
NORAD 67016
3.246 14.76 5.0e-06
2026-10-14 09:48:24 RROCI-2
NORAD 59106
STRIX-9
NORAD 100561
2.819 12.91 3.3e-07
2026-10-14 10:49:59 YAOGAN-30 03C
NORAD 43030
RROCI-2
NORAD 59106
0.856 13.74 3.1e-06
2026-10-14 11:24:52 STARLINK-5607
NORAD 55404
RROCI-2
NORAD 59106
4.063 15.02 2.9e-06
2026-10-14 11:51:03 STARLINK-6045
NORAD 56462
RROCI-2
NORAD 59106
3.114 14.52 5.9e-06
2026-10-14 20:55:27 STARLINK-3095
NORAD 49160
RROCI-2
NORAD 59106
2.700 6.19 1.7e-05
2026-10-15 15:00:21 RROCI-2
NORAD 59106
STARLINK-36172
NORAD 67020
3.612 14.88 3.8e-06
2026-10-15 15:41:10 YAOGAN-30 09B
NORAD 48424
RROCI-2
NORAD 59106
2.343 9.09 6.6e-07
2026-10-15 16:36:20 RROCI-2
NORAD 59106
STARLINK-35913
NORAD 67004
3.696 14.88 3.7e-06
2026-10-16 02:11:58 STARLINK-5835
NORAD 55772
RROCI-2
NORAD 59106
3.323 5.64 1.1e-05
2026-10-16 10:38:43 YAOGAN-30 07A
NORAD 45460
RROCI-2
NORAD 59106
2.226 12.97 5.3e-07
2026-10-16 12:51:44 RROCI-2
NORAD 59106
STARLINK-36230
NORAD 67075
2.996 12.81 9.0e-06
2026-10-16 15:02:55 STARLINK-5640
NORAD 55436
RROCI-2
NORAD 59106
3.225 14.73 5.1e-06
2026-10-17 08:04:53 STARLINK-5963
NORAD 56780
RROCI-2
NORAD 59106
4.123 10.19 6.1e-06

Data: CelesTrak SOCRATES Plus, computed from TLEs of the public catalog. This is an estimate, not grounds for a manoeuvre: TLEs carry no covariance, and the maximum probability assumes a position error.

All conjunctions of this satellite