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CUBEBUG-2

In orbit NORAD 39440 MRQX-2618-0103-4345-3937 Argentina

2013

Launch

1042

Observations all time

Mission information
Spacecraft name
CUBEBUG-2
Other names
LO-74
Status
Active
The satellite is in orbit
The network has not received data from this satellite for a long time
Launch and timeline
Launch time
2013-11-21 00:00:00
Separation time
Last observers
Observer
Time of receipt
Satellite appearance
Data for the last 30 days
Orbital parameters of the satellite
Perigee
541.52 km
Apogee
620.88 km
Inclination
97.9°
Period
96.4 min
Semi-major axis
6959.3 km
Velocity
7.52 km/s
Orbital elements
TLE source
Celestrak
TLE updated
2026-10-11 04:56:36 UTC
Two-line elements (TLE)
1 39440U 13066AA  26283.65491927  .00004125  00000-0  37643-3 0  9998
2 39440 97.9028 233.2432 0057021 5.8643 354.3232 14.94418379694233
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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 00:51:02 CUBEBUG-2 (LO-74)
NORAD 39440
ORBCOMM FM38
NORAD 33060
4.583 9.04 1.7e-07
2026-10-12 17:13:03 CUBEBUG-2 (LO-74)
NORAD 39440
STARLINK-5069
NORAD 55640
4.527 13.27 3.7e-06
2026-10-13 00:13:18 CUBEBUG-2 (LO-74)
NORAD 39440
CZ-4B DEB
NORAD 26329
4.963 14.63 7.5e-08
2026-10-13 01:05:33 CUBEBUG-2 (LO-74)
NORAD 39440
CZ-6A DEB
NORAD 55556
3.920 13.51 1.5e-07
2026-10-13 02:51:35 CUBEBUG-2 (LO-74)
NORAD 39440
STARLINK-5480
NORAD 55664
0.956 11.81 9.9e-05
2026-10-13 21:18:42 CUBEBUG-2 (LO-74)
NORAD 39440
DELTA 1 DEB
NORAD 9003
4.955 12.95 1.1e-07
2026-10-14 06:54:24 CUBEBUG-2 (LO-74)
NORAD 39440
ION SCV-023
NORAD 69876
4.470 6.60 2.0e-07
2026-10-14 08:35:27 CUBEBUG-2 (LO-74)
NORAD 39440
FENGYUN 1C DEB
NORAD 30569
4.885 13.95 9.1e-08
2026-10-14 08:35:36 CUBEBUG-2 (LO-74)
NORAD 39440
SL-16 DEB
NORAD 22455
1.737 14.32 6.6e-07
2026-10-14 16:24:25 CUBEBUG-2 (LO-74)
NORAD 39440
STARLINK-35763
NORAD 67089
3.372 7.66 1.0e-05
2026-10-14 18:03:19 CUBEBUG-2 (LO-74)
NORAD 39440
STARLINK-6292
NORAD 56775
3.277 13.48 6.8e-06
2026-10-15 16:15:07 CUBEBUG-2 (LO-74)
NORAD 39440
SL-16 DEB
NORAD 22327
4.854 15.13 6.5e-08
2026-10-15 17:51:14 CUBEBUG-2 (LO-74)
NORAD 39440
SL-16 DEB
NORAD 22327
4.105 15.13 9.0e-08
2026-10-15 19:27:22 CUBEBUG-2 (LO-74)
NORAD 39440
SL-16 DEB
NORAD 22327
3.674 15.13 1.1e-07
2026-10-15 21:03:30 CUBEBUG-2 (LO-74)
NORAD 39440
SL-16 DEB
NORAD 22327
3.716 15.13 1.1e-07
2026-10-15 22:39:37 CUBEBUG-2 (LO-74)
NORAD 39440
SL-16 DEB
NORAD 22327
4.232 15.13 8.5e-08
2026-10-16 01:16:40 CUBEBUG-2 (LO-74)
NORAD 39440
KUIPER-00542
NORAD 69611
3.441 8.71 3.1e-07
2026-10-17 02:22:02 CUBEBUG-2 (LO-74)
NORAD 39440
SL-14 R/B
NORAD 12988
4.729 13.62 2.5e-07
2026-10-17 03:25:02 CUBEBUG-2 (LO-74)
NORAD 39440
ATLAS 5 CENTAUR R/B
NORAD 39475
3.604 3.97 3.3e-07
2026-10-17 09:43:09 CUBEBUG-2 (LO-74)
NORAD 39440
NOAA 16 DEB
NORAD 42345
3.633 14.15 1.6e-07
2026-10-17 14:19:26 CUBEBUG-2 (LO-74)
NORAD 39440
RUBIN-2 & SAFIR-M
NORAD 27605
0.382 13.48 1.6e-05
2026-10-17 17:31:27 CUBEBUG-2 (LO-74)
NORAD 39440
THOR ABLESTAR DEB
NORAD 351
3.525 14.34 1.6e-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