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SARAL

In orbit NORAD 39086 CVJK-7644-2588-4230-2659 ISRO France India

Time in UTC

16:36

Next pass · МАН РС(Я) ГЕОСКАН УКВ · 11°

92

Observations over 30 days

43%

Successful observations

28k

Frames, latest 2026-10-04 00:07 UTC

Data for the last 30 days
Orbital parameters of the satellite
Perigee
778.26 km
Apogee
780.04 km
Inclination
98.6°
Period
100.5 min
Semi-major axis
7157.3 km
Velocity
7.45 km/s
Orbital elements
TLE source
Celestrak
TLE updated
2026-10-10 12:56:46 UTC
Two-line elements (TLE)
1 39086U 13009A   26283.25827802  .00000056  00000-0  36643-4 0  9991
2 39086 98.5552 108.3924 0001246 346.0408 14.0742 14.32911502712081
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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
2026-10-10 17:34:01 SARAL
NORAD 39086
UNKNOWN
NORAD 82139
3.033 11.98 3.1e-07
2026-10-11 02:12:53 SARAL
NORAD 39086
COSMOS 1818
NORAD 17369
0.326 14.74 1.4e-03
2026-10-11 04:20:53 SARAL
NORAD 39086
CZ-6A DEB
NORAD 60658
4.884 14.33 7.9e-08
2026-10-11 06:04:41 SARAL
NORAD 39086
SAPPHIRE
NORAD 39088
2.439 1.08 7.4e-07
2026-10-11 09:39:27 SARAL
NORAD 39086
CZ-6A DEB
NORAD 54634
1.565 14.63 6.9e-07
2026-10-11 11:11:37 SARAL
NORAD 39086
COSMOS 1190
NORAD 11869
3.961 9.27 5.4e-07
2026-10-11 11:25:17 SARAL
NORAD 39086
CZ-6A DEB
NORAD 54468
4.991 14.75 6.5e-08
2026-10-11 12:26:10 SARAL
NORAD 39086
COSMOS 2251 DEB
NORAD 37089
4.856 14.85 6.4e-08
2026-10-11 18:43:48 SARAL
NORAD 39086
IRIDIUM 126
NORAD 42809
3.770 14.76 1.1e-07
2026-10-12 02:23:40 SARAL
NORAD 39086
SL-16 DEB
NORAD 29098
4.655 14.82 7.3e-08
2026-10-12 09:24:40 SARAL
NORAD 39086
CZ-6A DEB
NORAD 60679
2.798 14.86 1.9e-07
2026-10-12 22:22:02 SARAL
NORAD 39086
NOAA 16 DEB
NORAD 41413
1.650 12.76 9.6e-07
2026-10-13 01:23:34 SARAL
NORAD 39086
FENGYUN 1C DEB
NORAD 31721
4.773 14.76 7.4e-08
2026-10-13 05:54:33 SARAL
NORAD 39086
NOAA 16 DEB
NORAD 41413
4.979 12.73 1.1e-07
2026-10-13 17:34:41 SARAL
NORAD 39086
PEGASUS DEB
NORAD 39312
4.221 14.36 1.0e-07
2026-10-13 20:56:31 SARAL
NORAD 39086
IRIDIUM 107
NORAD 42960
3.973 13.82 1.4e-07
2026-10-14 07:58:13 SARAL
NORAD 39086
WEBERSAT (WO-18)
NORAD 20441
2.924 14.36 1.1e-07
2026-10-14 10:19:17 SARAL
NORAD 39086
IRIDIUM 148
NORAD 43255
2.500 13.40 3.7e-07
2026-10-14 14:42:06 SARAL
NORAD 39086
DMSP 5D-2 F13 DEB
NORAD 40447
2.830 14.51 2.2e-07
2026-10-14 18:39:12 SARAL
NORAD 39086
IRIDIUM 137
NORAD 43076
2.616 14.64 2.4e-07
2026-10-15 01:41:40 SARAL
NORAD 39086
DMSP 5D-2 F13 DEB
NORAD 40677
3.432 14.70 1.4e-07
2026-10-15 09:54:56 SARAL
NORAD 39086
IRIDIUM 167
NORAD 43931
2.135 14.83 3.3e-07
2026-10-15 12:17:48 SARAL
NORAD 39086
USA 81
NORAD 21949
0.571 12.19 8.6e-06
2026-10-15 12:19:52 SARAL
NORAD 39086
IRIDIUM 33 DEB
NORAD 46974
2.588 14.12 3.0e-07
2026-10-15 13:08:05 SARAL
NORAD 39086
USA 81
NORAD 21949
4.788 12.17 1.2e-07
2026-10-16 01:06:01 SARAL
NORAD 39086
FENGYUN 1C DEB
NORAD 35203
4.231 14.66 9.9e-08
2026-10-16 08:34:27 SARAL
NORAD 39086
FENGYUN 1C DEB
NORAD 31507
3.822 14.39 1.2e-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