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SKYMED 1

In orbit NORAD 31598 BEBS-6223-1179-9603-3761 United States of America

2007

Launch

0

Observations all time

Mission information
Spacecraft name
SKYMED 1
Other names
2007-023A
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
2007-06-08 00:00:00
Separation time
2007-06-08 00:00:00
Satellite appearance
Data for the last 30 days
Orbital parameters of the satellite
Perigee
570.67 km
Apogee
572.47 km
Inclination
97.9°
Period
96.2 min
Semi-major axis
6949.7 km
Velocity
7.56 km/s
Orbital elements
TLE source
Celestrak
TLE updated
2026-10-10 20:56:55 UTC
Two-line elements (TLE)
1 31598U 07023A   26283.61202590  .00002265  00000-0  19934-3 0  9998
2 31598 97.8799 116.4742 0001316 97.8551 262.2820 14.97523490 47061
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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 02:13:11 COSMO-SKYMED 1
NORAD 31598
THORAD AGENA D DEB
NORAD 4435
4.004 10.13 2.1e-07
2026-10-11 02:29:38 COSMO-SKYMED 1
NORAD 31598
STARLINK-5621
NORAD 55434
2.787 14.93 6.4e-06
2026-10-11 04:44:57 COSMO-SKYMED 1
NORAD 31598
FENGYUN 1C DEB
NORAD 35243
3.034 8.59 4.0e-07
2026-10-11 11:04:57 COSMO-SKYMED 1
NORAD 31598
GRAVITY-1 R/B
NORAD 100710
4.219 14.57 1.0e-07
2026-10-11 22:56:45 COSMO-SKYMED 1
NORAD 31598
STARLINK-34620
NORAD 64803
3.649 14.99 3.6e-06
2026-10-11 23:01:02 COSMO-SKYMED 1
NORAD 31598
STARLINK-5985
NORAD 56451
0.472 14.82 2.3e-04
2026-10-12 02:16:24 COSMO-SKYMED 1
NORAD 31598
STARLINK-5603
NORAD 55762
3.615 9.99 8.0e-06
2026-10-13 14:10:06 COSMO-SKYMED 1
NORAD 31598
STARLINK-3058
NORAD 49138
4.881 4.08 5.4e-06
2026-10-14 05:21:04 COSMO-SKYMED 1
NORAD 31598
STARLINK-34644
NORAD 64812
2.747 15.06 6.2e-06
2026-10-14 06:09:02 COSMO-SKYMED 1
NORAD 31598
STARLINK-34624
NORAD 64805
3.964 15.05 3.0e-06
2026-10-14 07:47:36 COSMO-SKYMED 1
NORAD 31598
FORMOSAT 7-4
NORAD 44350
4.024 12.00 1.8e-07
2026-10-14 14:42:26 SHIJIAN-6 02B (SJ-6 02B)
NORAD 29506
COSMO-SKYMED 1
NORAD 31598
3.481 14.85 1.4e-07
2026-10-14 18:25:41 COSMO-SKYMED 1
NORAD 31598
STARLINK-5501
NORAD 55648
4.928 13.66 2.9e-06
2026-10-14 20:01:52 COSMO-SKYMED 1
NORAD 31598
STARLINK-5501
NORAD 55648
4.616 13.67 3.3e-06
2026-10-14 21:30:05 COSMO-SKYMED 1
NORAD 31598
STARLINK-5986
NORAD 56452
2.850 15.00 5.9e-06
2026-10-15 02:08:23 COSMO-SKYMED 1
NORAD 31598
STARLINK-34649
NORAD 64798
3.543 15.06 3.7e-06
2026-10-15 06:45:25 COSMO-SKYMED 1
NORAD 31598
KAZSTSAT
NORAD 43783
2.594 14.88 2.4e-07
2026-10-15 07:17:07 COSMO-SKYMED 1
NORAD 31598
FENGYUN 1C DEB
NORAD 30290
4.063 10.86 2.0e-07
2026-10-15 22:07:32 COSMO-SKYMED 1
NORAD 31598
STARLINK-34696
NORAD 64808
3.898 15.06 3.1e-06
2026-10-16 07:13:05 COSMO-SKYMED 1
NORAD 31598
STARLINK-5909
NORAD 55938
1.279 5.62 7.6e-05
2026-10-16 14:30:27 COSMO-SKYMED 1
NORAD 31598
SL-12 R/B(AUX MOTOR)
NORAD 33472
4.769 13.84 1.3e-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