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Centauri-9

In orbit NORAD 69924 XKIE-9046-7891-3526-0246

Falcon 9 Block 5

Carrier rocket

Space Launch Complex 4E

Spaceport

51

Observations all time

Mission information
Spacecraft name
Centauri-9
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
2026-07-07 07:12:00
Separation time
2026-07-07 08:09:06
Satellite appearance
Data for the last 30 days
Orbital parameters of the satellite
Perigee
582.51 km
Apogee
593.37 km
Inclination
97.7°
Period
96.5 min
Semi-major axis
6966.1 km
Velocity
7.56 km/s
Orbital elements
TLE source
Celestrak
TLE updated
2026-10-10 20:57:00 UTC
Two-line elements (TLE)
1 69924U 26156BH  26283.22839382  .00000697  00000-0  73828-4 0  9992
2 69924 97.7420 182.1200 0007838 187.7942 172.3156 14.92250280 14158
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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
2026-10-11 17:03:17 ARCTIC WEATHER SATELLITE
NORAD 60543
CENTAURI-9
NORAD 69924
4.977 14.91 6.6e-08
2026-10-12 01:17:40 LEMUR-2-HCS-BAZUS
NORAD 67388
CENTAURI-9
NORAD 69924
0.918 11.38 3.7e-06
2026-10-12 04:52:29 CENTAURI-9
NORAD 69924
CZ-6A DEB
NORAD 54576
2.960 14.96 1.8e-07
2026-10-12 05:13:04 CENTAURI-9
NORAD 69924
DELTA 1 DEB
NORAD 26828
4.667 14.49 8.7e-08
2026-10-12 06:49:38 CENTAURI-9
NORAD 69924
DELTA 1 DEB
NORAD 26828
1.171 14.49 1.4e-06
2026-10-12 08:26:12 CENTAURI-9
NORAD 69924
DELTA 1 DEB
NORAD 26828
4.839 14.49 8.1e-08
2026-10-12 10:51:05 CENTAURI-9
NORAD 69924
DELTA 1 DEB
NORAD 26828
4.048 14.50 1.2e-07
2026-10-12 12:31:14 CENTAURI-9
NORAD 69924
FENGYUN 1C DEB
NORAD 30884
4.724 13.63 1.0e-07
2026-10-12 12:31:55 CENTAURI-9
NORAD 69924
COSMOS 2251 DEB
NORAD 34681
3.088 14.11 2.2e-07
2026-10-12 13:29:02 CENTAURI-9
NORAD 69924
CZ-4B DEB
NORAD 26220
3.544 13.65 1.8e-07
2026-10-12 16:05:06 CENTAURI-9
NORAD 69924
FENGYUN 1C DEB
NORAD 30971
4.132 14.95 9.6e-08
2026-10-14 02:18:30 CENTAURI-9
NORAD 69924
PEGASUS DEB
NORAD 39322
3.696 15.17 1.1e-07
2026-10-14 19:03:47 O/OREOS (USA 219)
NORAD 37224
CENTAURI-9
NORAD 69924
3.038 4.03 4.6e-07
2026-10-15 08:11:25 PEARL-1B
NORAD 68980
CENTAURI-9
NORAD 69924
1.106 0.52 3.6e-06
2026-10-15 14:37:07 JACK E
NORAD 66654
CENTAURI-9
NORAD 69924
4.693 3.70 2.0e-07
2026-10-16 00:16:24 LEMUR-2-DELOITTE-5
NORAD 69910
CENTAURI-9
NORAD 69924
2.925 0.02 5.2e-07
2026-10-16 14:10:17 CENTAURI-9
NORAD 69924
COSMOS 2251 DEB
NORAD 37968
3.235 15.00 1.5e-07
2026-10-16 21:38:08 CENTAURI-9
NORAD 69924
DELTA 2 R/B(1)
NORAD 21891
2.321 12.88 2.4e-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