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DUBAISAT 1

In orbit NORAD 35682 THDC-5854-7345-5323-0312 United Arab Emirates

Observations 0
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2009

Launch

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Observations all time

Mission information
Spacecraft name
DUBAISAT 1
Other names
2009-041B
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
2009-07-29 00:00:00
Separation time
2009-07-29 00:00:00
Satellite appearance
Data for the last 30 days
Orbital parameters of the satellite
Perigee
633.23 km
Apogee
649.37 km
Inclination
98.0°
Period
97.6 min
Semi-major axis
7019.4 km
Velocity
7.54 km/s
Orbital elements
TLE source
Celestrak
TLE updated
2026-10-11 04:56:36 UTC
Two-line elements (TLE)
1 35682U 09041B   26283.93949170  .00000870  00000-0  13587-3 0  9993
2 35682  98.0220  56.0521 0011497  63.1221 297.1162 14.75284573922167
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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
2026-10-11 18:33:06 DUBAISAT-1
NORAD 35682 		FENGYUN 1C DEB
NORAD 38169 		0.719 12.85 5.1e-06
2026-10-12 01:51:46 DUBAISAT-1
NORAD 35682 		CZ-6A DEB
NORAD 61331 		1.860 14.42 5.4e-07
2026-10-12 08:20:31 DUBAISAT-1
NORAD 35682 		FENGYUN 1C DEB
NORAD 30624 		3.951 2.39 2.8e-07
2026-10-13 10:23:39 DUBAISAT-1
NORAD 35682 		CZ-6A DEB
NORAD 54444 		3.900 7.81 2.5e-07
2026-10-14 00:53:05 DUBAISAT-1
NORAD 35682 		COSMOS 2251 DEB
NORAD 35980 		4.372 14.88 8.4e-08
2026-10-15 05:35:13 DUBAISAT-1
NORAD 35682 		USA 57
NORAD 20561 		1.753 14.77 5.5e-07
2026-10-15 13:57:01 DUBAISAT-1
NORAD 35682 		IRIDIUM 33 DEB
NORAD 34696 		4.326 15.04 7.9e-08
2026-10-16 00:16:21 DUBAISAT-1
NORAD 35682 		DMSP 5D-2 F14 DEB
NORAD 62944 		3.161 11.95 2.9e-07
2026-10-16 03:29:50 DUBAISAT-1
NORAD 35682 		CZ-6A DEB
NORAD 54412 		1.570 1.55 1.8e-06
2026-10-17 02:57:27 DUBAISAT-1
NORAD 35682 		DELTA 1 DEB
NORAD 8951 		3.000 14.43 2.1e-07
2026-10-17 05:42:26 DUBAISAT-1
NORAD 35682 		CZ-6A DEB
NORAD 61419 		3.613 14.97 1.2e-07
2026-10-17 07:46:46 DUBAISAT-1
NORAD 35682 		CZ-6A DEB
NORAD 61307 		4.264 15.06 8.3e-08

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