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SKYMED 2

In orbit NORAD 32376 JXWR-7717-8415-0462-5029 Italy

2007

Launch

1

Observations all time

Mission information
Spacecraft name
SKYMED 2
Other names
2007-059A
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
2007-12-09 00:00:00
Separation time
2007-12-09 00:00:00
Satellite appearance
Data for the last 30 days
Orbital parameters of the satellite
Perigee
618.60 km
Apogee
620.54 km
Inclination
97.9°
Period
97.2 min
Semi-major axis
6997.7 km
Velocity
7.53 km/s
Orbital elements
TLE source
Celestrak
TLE updated
2026-10-13 06:09:00 UTC
Two-line elements (TLE)
1 32376U 07059A   26285.96701191  .00000390  00000-0  55562-4 0  9998
2 32376 97.8902 107.8951 0001390 90.8664 269.2709 14.82153781 19459
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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
2026-10-13 10:18:47 COSMO-SKYMED 2
NORAD 32376
KUIPER-00024
NORAD 63738
4.749 11.90 1.3e-07
2026-10-13 10:19:19 COSMO-SKYMED 2
NORAD 32376
GEESAT-5 07
NORAD 65556
4.414 11.90 1.5e-07
2026-10-13 11:23:16 COSMO-SKYMED 2
NORAD 32376
KUIPER-00118
NORAD 65154
4.461 14.56 9.2e-08
2026-10-13 17:30:04 COSMO-SKYMED 2
NORAD 32376
UNKNOWN
NORAD 270440
4.939 14.69 7.3e-08
2026-10-13 22:52:44 COSMO-SKYMED 2
NORAD 32376
AEROCUBE 2
NORAD 31133
2.272 14.85 3.2e-07
2026-10-14 02:10:38 COSMO-SKYMED 2
NORAD 32376
KUIPER-00094
NORAD 64839
4.782 12.18 1.2e-07
2026-10-15 11:09:34 COSMO-SKYMED 2
NORAD 32376
DELTA 1 R/B(1)
NORAD 10954
3.868 8.73 2.4e-07
2026-10-15 20:24:36 COSMO-SKYMED 2
NORAD 32376
COSMOS 2251 DEB
NORAD 34482
4.344 13.43 1.3e-07
2026-10-15 20:54:04 COSMO-SKYMED 2
NORAD 32376
NOAA 17 DEB
NORAD 48702
4.571 14.94 7.6e-08
2026-10-16 08:32:14 COSMO-SKYMED 2
NORAD 32376
SL-16 DEB
NORAD 39886
3.609 10.45 2.6e-07
2026-10-17 01:18:55 COSMO-SKYMED 2
NORAD 32376
KUIPER-00214
NORAD 67778
4.195 14.49 1.1e-07
2026-10-17 07:45:31 COSMO-SKYMED 2
NORAD 32376
COSMOS 2251 DEB
NORAD 35611
3.581 15.05 1.2e-07
2026-10-17 09:30:38 COSMO-SKYMED 2
NORAD 32376
KUIPER-00058
NORAD 64518
4.061 14.06 1.3e-07
2026-10-17 20:53:28 COSMO-SKYMED 2
NORAD 32376
KUIPER-00511
NORAD 68888
4.124 9.41 2.1e-07
2026-10-17 21:28:10 COSMO-SKYMED 2
NORAD 32376
SL-14 R/B
NORAD 17192
1.888 15.09 9.8e-07
2026-10-18 00:29:27 COSMO-SKYMED 2
NORAD 32376
KUIPER-00562
NORAD 69270
4.930 11.41 1.3e-07
2026-10-18 06:03:29 COSMO-SKYMED 2
NORAD 32376
DELTA 1 DEB
NORAD 42556
2.160 13.20 5.4e-07
2026-10-18 06:55:16 COSMO-SKYMED 2
NORAD 32376
COSMOS 2251 DEB
NORAD 34972
3.488 6.87 3.3e-07
2026-10-18 12:39:24 COSMO-SKYMED 2
NORAD 32376
GEESAT-3 08
NORAD 61018
4.498 12.80 1.3e-07
2026-10-18 22:45:20 COSMO-SKYMED 2
NORAD 32376
KUIPER-00061
NORAD 64521
4.542 14.22 9.8e-08
2026-10-18 23:46:08 COSMO-SKYMED 2
NORAD 32376
PROITERES
NORAD 38756
2.484 11.75 4.9e-07
2026-10-19 03:49:10 COSMO-SKYMED 2
NORAD 32376
PROITERES
NORAD 38756
1.429 11.72 1.5e-06

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