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GOMX 1

In orbit NORAD 39430 ZFJP-4482-3637-6524-3782 Denmark

Time in UTC

01:38

Next pass · Индия · 51°

—

No observations scheduled

1

Observations over 30 days

85%

Successful observations

14k

Frames, latest 2026-10-05 00:53 UTC

Mission information
Spacecraft name
GOMX 1
Other names
GATOSS
Status
Active
The satellite is in orbit
Launch and timeline
Launch time
2013-11-21 00:00:00
Separation time
Last observers
Observer
Time of receipt
2026-06-18 17:01:13 UTC
2026-02-13 12:52:15 UTC
2025-08-05 00:09:58 UTC
2025-07-25 04:14:25 UTC
Satellite appearance
Data for the last 30 days
Orbital parameters of the satellite
Perigee
567.84 km
Apogee
749.94 km
Inclination
97.6°
Period
98.0 min
Semi-major axis
7037.0 km
Velocity
7.62 km/s
Orbital elements
TLE source
Celestrak
TLE updated
2026-10-10 20:56:55 UTC
Two-line elements (TLE)
1 39430U 13066Q   26283.59266873  .00000906  00000-0  14112-3 0  9999
2 39430 97.6411 116.7788 0129380 66.7494 294.7274 14.69755790686868
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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 01:46:32 GOMX-1
NORAD 39430
RCM-1
NORAD 44322
1.693 15.00 5.6e-07
2026-10-11 02:46:40 GOMX-1
NORAD 39430
SL-8 DEB
NORAD 25563
0.091 7.70 4.7e-04
2026-10-11 06:09:35 GOMX-1
NORAD 39430
UNKNOWN
NORAD 270425
3.450 10.21 2.8e-07
2026-10-11 10:03:45 GOMX-1
NORAD 39430
STARLINK-5911
NORAD 55950
0.385 5.90 8.4e-04
2026-10-11 10:05:30 GOMX-1
NORAD 39430
STARLINK-5986
NORAD 56452
2.968 14.82 6.0e-06
2026-10-11 21:34:50 GOMX-1
NORAD 39430
STARLINK-36239
NORAD 67196
3.111 13.70 7.3e-06
2026-10-12 01:49:39 GOMX-1
NORAD 39430
COSMOS 2251 DEB
NORAD 34127
4.973 11.29 1.3e-07
2026-10-12 05:47:59 GOMX-1
NORAD 39430
CZ-2C DEB
NORAD 39204
1.513 10.74 1.4e-06
2026-10-13 00:37:23 GOMX-1
NORAD 39430
CZ-6A DEB
NORAD 60765
1.259 12.54 1.7e-06
2026-10-13 07:32:11 GOMX-1
NORAD 39430
KUIPER-00611
NORAD 69771
3.204 5.96 4.0e-07
2026-10-13 08:51:00 GOMX-1
NORAD 39430
FENGYUN 1C DEB
NORAD 30001
4.161 11.21 1.8e-07
2026-10-13 13:40:11 GOMX-1
NORAD 39430
CZ-6A DEB
NORAD 60784
2.977 13.98 2.3e-07
2026-10-14 08:21:59 GOMX-1
NORAD 39430
STARLINK-3060
NORAD 49155
1.671 7.90 4.2e-05
2026-10-14 09:56:05 GOMX-1
NORAD 39430
ORBCOMM FM02
NORAD 23546
1.373 14.99 2.5e-06
2026-10-14 12:21:49 GOMX-1
NORAD 39430
FENGYUN 1C DEB
NORAD 29845
4.973 14.64 6.8e-08
2026-10-14 14:10:35 GOMX-1
NORAD 39430
CZ-6A DEB
NORAD 60871
2.669 14.02 2.8e-07
2026-10-15 07:10:13 GOMX-1
NORAD 39430
STARLINK-5909
NORAD 55938
4.689 5.29 5.7e-06
2026-10-15 11:31:14 GOMX-1
NORAD 39430
COSMOS 2251 DEB
NORAD 34122
0.792 13.28 3.8e-06
2026-10-15 16:20:10 GOMX-1
NORAD 39430
METEOR 2-5 DEB
NORAD 38280
3.932 14.33 1.2e-07
2026-10-15 19:57:25 GOMX-1
NORAD 39430
GEESAT-4 08
NORAD 65126
0.970 14.43 2.0e-06
2026-10-16 03:05:14 GOMX-1
NORAD 39430
DMSP 5D-3 F16 DEB
NORAD 28081
4.163 14.41 1.1e-07
2026-10-16 21:02:11 GOMX-1
NORAD 39430
TYVAK-0173
NORAD 48892
1.630 14.38 7.3e-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