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ADDCUBE

In orbit NORAD 64590 SSSX-0322-2102-6904-8277

Falcon 9 Block 5

Carrier rocket

Space Launch Complex 4E

Spaceport

21

Observations all time

Mission information
Spacecraft name
ADDCUBE
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
2025-06-23 21:25:00
Separation time
2025-06-23 23:41:16
Satellite appearance
Data for the last 30 days
Orbital parameters of the satellite
Perigee
578.32 km
Apogee
584.38 km
Inclination
97.8°
Period
96.4 min
Semi-major axis
6959.5 km
Velocity
7.57 km/s
Orbital elements
TLE source
Celestrak
TLE updated
2026-10-11 12:56:45 UTC
Two-line elements (TLE)
1 64590U 25135BQ  26283.57334420  .00001393  00000-0  13482-3 0  9996
2 64590 97.7823 36.8916 0004335 319.7944 40.2954 14.94372305 71131
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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 03:08:01 TRANSPORTER-14 OBJECT BQ
NORAD 64590
PEARL-1B
NORAD 68980
3.623 14.16 1.6e-07
2026-10-13 05:48:51 TRANSPORTER-14 OBJECT BQ
NORAD 64590
FENGYUN 1C DEB
NORAD 31883
2.638 14.76 2.5e-07
2026-10-14 07:18:20 TRANSPORTER-14 OBJECT BQ
NORAD 64590
DELTA 1 DEB
NORAD 12227
2.285 11.45 5.9e-07
2026-10-14 07:59:59 TRANSPORTER-14 OBJECT BQ
NORAD 64590
FENGYUN 1C DEB
NORAD 30879
4.614 14.65 8.5e-08
2026-10-14 22:49:36 TRANSPORTER-14 OBJECT BQ
NORAD 64590
ORBCOMM FM111
NORAD 40089
4.329 13.28 1.3e-07
2026-10-15 22:37:22 TRANSPORTER-14 OBJECT BQ
NORAD 64590
CESARIO
NORAD 100642
1.844 14.27 5.9e-07
2026-10-16 14:47:32 ARVAKER-3
NORAD 64566
TRANSPORTER-14 OBJECT BQ
NORAD 64590
1.710 0.05 1.5e-06
2026-10-16 15:35:50 ARVAKER-3
NORAD 64566
TRANSPORTER-14 OBJECT BQ
NORAD 64590
3.897 0.05 2.9e-07
2026-10-16 18:02:26 TRANSPORTER-14 OBJECT BQ
NORAD 64590
FGN-TUG-S01
NORAD 100399
4.894 10.92 1.4e-07
2026-10-17 05:34:22 TRANSPORTER-14 OBJECT BQ
NORAD 64590
OBJECT G
NORAD 59884
4.876 6.51 1.7e-07
2026-10-17 18:00:24 TRANSPORTER-14 OBJECT BQ
NORAD 64590
ICEYE-X77
NORAD 69892
2.190 14.32 4.2e-07
2026-10-17 19:44:08 TRANSPORTER-14 OBJECT BQ
NORAD 64590
CZ-6A DEB
NORAD 54576
2.885 3.69 5.2e-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