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CUBY-3

In orbit NORAD 69875 FHJG-9089-0997-9355-3963

Falcon 9 Block 5

Carrier rocket

Space Launch Complex 4E

Spaceport

6

Observations all time

Mission information
Spacecraft name
CUBY-3
Frequency usage status
Violator
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 08:08:52
Satellite appearance
Data for the last 30 days
Orbital parameters of the satellite
Perigee
588.74 km
Apogee
594.33 km
Inclination
97.7°
Period
96.6 min
Semi-major axis
6969.7 km
Velocity
7.54 km/s
Orbital elements
TLE source
Celestrak
TLE updated
2026-10-11 12:56:46 UTC
Two-line elements (TLE)
1 69875U 26156G   26284.17570205  .00001754  00000-0  18254-3 0  9994
2 69875 97.7409 182.8606 0003955 145.0849 215.0629 14.91096073 14287
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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
2026-10-13 10:55:04 CUBY-3
NORAD 69875
CZ-6A DEB
NORAD 54629
4.866 14.97 6.7e-08
2026-10-13 12:31:21 CUBY-3
NORAD 69875
FENGYUN 1C DEB
NORAD 38783
4.750 15.00 7.0e-08
2026-10-13 13:45:33 CUBY-3
NORAD 69875
FENGYUN 1C DEB
NORAD 29866
2.822 10.21 4.3e-07
2026-10-13 18:35:43 SJ-9B
NORAD 38861
CUBY-3
NORAD 69875
2.323 9.74 6.5e-07
2026-10-13 21:00:42 SJ-9B
NORAD 38861
CUBY-3
NORAD 69875
2.967 9.77 4.0e-07
2026-10-14 00:42:48 FIREFLY-3
NORAD 62710
CUBY-3
NORAD 69875
3.635 14.98 1.2e-07
2026-10-14 02:19:22 FIREFLY-3
NORAD 62710
CUBY-3
NORAD 69875
3.970 14.98 1.0e-07
2026-10-14 05:53:52 ICEYE-X78
NORAD 68995
CUBY-3
NORAD 69875
2.894 0.45 5.3e-07
2026-10-14 15:02:57 CUBY-3
NORAD 69875
CBERS 1 DEB
NORAD 35387
0.568 14.95 5.0e-06
2026-10-14 16:39:32 CUBY-3
NORAD 69875
CBERS 1 DEB
NORAD 35387
4.501 14.95 7.9e-08
2026-10-14 19:18:01 CAPELLA-11 (ACADIA-1)
NORAD 57693
CUBY-3
NORAD 69875
2.291 14.50 3.6e-07
2026-10-14 20:43:51 CUBY-3
NORAD 69875
CZ-6A DEB
NORAD 55232
1.560 14.97 6.6e-07
2026-10-15 02:01:10 CUBY-3
NORAD 69875
SL-8 R/B
NORAD 20775
2.483 13.93 1.8e-06
2026-10-15 11:47:54 IRIDE-MS2-HEO-9
NORAD 64585
CUBY-3
NORAD 69875
2.978 14.32 2.2e-07
2026-10-15 13:19:53 CUBY-3
NORAD 69875
SICH-1
NORAD 23657
2.144 11.66 8.6e-06
2026-10-15 18:58:50 CUBY-3
NORAD 69875
CZ-2D DEB
NORAD 44611
0.627 11.05 8.1e-06
2026-10-16 07:00:38 OBJECT C
NORAD 66652
CUBY-3
NORAD 69875
2.008 3.72 1.1e-06
2026-10-16 07:12:03 CUBY-3
NORAD 69875
LIJIAN-1 R/B
NORAD 66411
2.981 14.76 1.9e-07
2026-10-16 08:38:54 CUBY-3
NORAD 69875
FENGYUN 1C DEB
NORAD 30232
4.328 4.69 2.3e-07
2026-10-17 23:15:48 SERT3
NORAD 68499
CUBY-3
NORAD 69875
4.988 7.24 1.6e-07
2026-10-18 00:04:06 SERT3
NORAD 68499
CUBY-3
NORAD 69875
3.799 7.23 2.7e-07

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