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QUBE

In orbit NORAD 60476 ZYDE-4447-8719-9309-2022 Germany

Falcon 9 Block 5

Carrier rocket

Space Launch Complex 4E

Spaceport

0

Observations all time

Mission information
Spacecraft name
QUBE
Other names
DP2QU
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
2024-08-16 18:56:00
Separation time
2024-08-16 19:56:08
Satellite appearance
Data for the last 30 days
Orbital parameters of the satellite
Perigee
402.88 km
Apogee
407.00 km
Inclination
97.4°
Period
92.7 min
Semi-major axis
6782.9 km
Velocity
7.65 km/s
Orbital elements
TLE source
Celestrak
TLE updated
2026-10-13 14:09:03 UTC
Two-line elements (TLE)
1 60476U 24149J   26286.25140265  .00033688  00000-0  53921-3 0  9993
2 60476 97.3742 15.4171 0003036 139.4588 220.6891 15.53055890120750
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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
2026-10-14 23:31:03 QUBE
NORAD 60476
STARLINK-38413
NORAD 100635
2.523 14.80 8.6e-06
2026-10-16 01:47:33 QUBE
NORAD 60476
STARLINK-38422
NORAD 100637
1.516 14.66 2.5e-05
2026-10-16 04:53:03 QUBE
NORAD 60476
STARLINK-38421
NORAD 100631
4.522 14.65 2.8e-06
2026-10-16 11:03:59 QUBE
NORAD 60476
STARLINK-38415
NORAD 100634
1.669 14.61 2.1e-05
2026-10-18 04:48:00 QUBE
NORAD 60476
STARLINK-36778
NORAD 100627
4.187 14.36 3.6e-06
2026-10-18 05:00:44 QUBE
NORAD 60476
COSMOS 2251 DEB
NORAD 33821
2.661 15.28 2.1e-07
2026-10-18 20:57:26 SKYSAT-C12
NORAD 43797
QUBE
NORAD 60476
2.405 8.81 3.6e-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