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FUNCUBE-1

In orbit NORAD 39444 OTOF-8025-8953-4756-4779

Time in UTC

02:12

Next pass · Обозерский

—

No observations scheduled

53

Observations over 30 days

43%

Successful observations

34k

Frames, latest 2026-09-27 20:24 UTC

Mission information
Spacecraft name
FUNCUBE-1
Other names
AO-73
Status
Active
The satellite is in orbit
Launch and timeline
Launch time
2013-11-21 00:00:00
Separation time
Satellite appearance
Data for the last 30 days
Orbital parameters of the satellite
Perigee
506.20 km
Apogee
555.10 km
Inclination
97.8°
Period
95.3 min
Semi-major axis
6908.8 km
Velocity
7.62 km/s
Orbital elements
TLE source
Celestrak
TLE updated
2026-10-10 04:46:17 UTC
Two-line elements (TLE)
1 39444U 13066AE  26282.88258682  .00006914  00000-0  41381-3 0  9997
2 39444 97.8418 256.9310 0035386 170.1863 190.0065 15.10834091696970
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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 04:17:41 FUNCUBE-1 (AO-73)
NORAD 39444
CURIUM ONE
NORAD 60242
3.819 12.41 1.9e-07
2026-10-14 07:41:23 FUNCUBE-1 (AO-73)
NORAD 39444
YAOGAN-30 08A
NORAD 46807
3.892 13.89 1.5e-07
2026-10-15 06:09:23 FUNCUBE-1 (AO-73)
NORAD 39444
STARLINK-5471
NORAD 54766
2.577 13.31 1.1e-05
2026-10-16 03:44:19 FUNCUBE-1 (AO-73)
NORAD 39444
OBJECT E
NORAD 69101
2.640 11.97 4.2e-07
2026-10-16 14:09:22 FUNCUBE-1 (AO-73)
NORAD 39444
STARLINK-4380
NORAD 53650
4.531 11.70 4.5e-06
2026-10-16 16:27:13 FUNCUBE-1 (AO-73)
NORAD 39444
OBJECT J
NORAD 100137
3.847 11.99 2.0e-07
2026-10-16 18:02:35 FUNCUBE-1 (AO-73)
NORAD 39444
OBJECT J
NORAD 100137
2.756 11.99 3.9e-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