RU | EN | ZH --:-- UTC Sign in

UMBRA-12

In orbit NORAD 67371 WITJ-6949-7336-2913-9918

Falcon 9 Block 5

Carrier rocket

Space Launch Complex 4E

Spaceport

0

Observations all time

Mission information
Spacecraft name
UMBRA-12
Status
Active
The satellite is in orbit
The network has not received data from this satellite for a long time
Launch and timeline
Carrier rocket
Falcon 9 Block 5
Spaceport
Space Launch Complex 4E
Launch time
Separation time
Satellite appearance
Data for the last 30 days
Orbital parameters of the satellite
Perigee
589.47 km
Apogee
599.79 km
Inclination
97.8°
Period
96.6 min
Semi-major axis
6972.8 km
Velocity
7.54 km/s
Orbital elements
TLE source
Celestrak
TLE updated
2026-10-11 12:56:45 UTC
Two-line elements (TLE)
1 67371U 26004J   26284.23949690  .00004691  00000-0  49062-3 0  9994
2 67371 97.8067 281.5137 0007399 105.7519 254.4515 14.90106912 40582
Copy content
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
2026-10-12 04:40:13 UMBRA-12
NORAD 67371
CZ-4B DEB
NORAD 26272
4.205 11.38 1.8e-07
2026-10-12 04:45:08 UMBRA-12
NORAD 67371
CUBY-5
NORAD 69907
0.946 11.37 3.5e-06
2026-10-12 22:31:53 UMBRA-12
NORAD 67371
COSMOS 2251 DEB
NORAD 35445
3.687 14.79 1.3e-07
2026-10-13 00:05:29 UMBRA-12
NORAD 67371
TOM-3
NORAD 69906
4.764 11.37 1.4e-07
2026-10-13 16:04:20 UMBRA-12
NORAD 67371
CZ-4C DEB
NORAD 37569
3.170 14.11 2.1e-07
2026-10-13 16:12:26 UMBRA-12
NORAD 67371
IPOS-TDSM
NORAD 69913
4.182 11.36 1.8e-07
2026-10-14 12:40:45 UMBRA-12
NORAD 67371
FALCON 1 R/B
NORAD 35579
3.228 11.05 3.1e-07
2026-10-14 18:43:41 UMBRA-12
NORAD 67371
CZ-6A DEB
NORAD 54471
1.998 9.08 9.1e-07
2026-10-15 02:02:04 OBJECT C
NORAD 66652
UMBRA-12
NORAD 67371
2.077 8.58 8.6e-07
2026-10-15 06:07:10 YAOGAN-2
NORAD 31490
UMBRA-12
NORAD 67371
4.844 13.69 9.7e-08
2026-10-16 01:33:49 GEESAT-1 06
NORAD 52790
UMBRA-12
NORAD 67371
1.139 10.32 2.6e-06
2026-10-16 19:01:27 UMBRA-12
NORAD 67371
PEGASUS R/B
NORAD 27859
4.490 9.63 1.7e-07
2026-10-16 20:33:58 UMBRA-12
NORAD 67371
DUMMY MASS 1
NORAD 24925
1.544 2.68 1.8e-06
2026-10-17 07:12:34 UMBRA-12
NORAD 67371
SL-14 R/B
NORAD 12988
3.302 15.13 3.2e-07
2026-10-17 08:49:21 UMBRA-12
NORAD 67371
SL-14 R/B
NORAD 12988
1.693 15.13 1.2e-06
2026-10-17 10:26:08 UMBRA-12
NORAD 67371
SL-14 R/B
NORAD 12988
0.780 15.13 5.8e-06
2026-10-17 12:02:55 UMBRA-12
NORAD 67371
SL-14 R/B
NORAD 12988
1.574 15.13 1.4e-06
2026-10-17 12:03:59 UMBRA-12
NORAD 67371
GRUS-3D
NORAD 69919
3.883 11.36 2.1e-07
2026-10-17 13:39:42 UMBRA-12
NORAD 67371
SL-14 R/B
NORAD 12988
2.648 15.13 5.0e-07
2026-10-17 15:16:29 UMBRA-12
NORAD 67371
SL-14 R/B
NORAD 12988
3.598 15.13 2.7e-07
2026-10-17 16:53:16 UMBRA-12
NORAD 67371
SL-14 R/B
NORAD 12988
4.384 15.13 1.8e-07
2026-10-17 16:54:03 UMBRA-12
NORAD 67371
POSIDONIA
NORAD 69922
2.095 11.36 7.1e-07
2026-10-17 18:30:03 UMBRA-12
NORAD 67371
SL-14 R/B
NORAD 12988
4.995 15.13 1.4e-07
2026-10-18 04:10:45 UMBRA-12
NORAD 67371
SL-14 R/B
NORAD 12988
4.917 15.13 1.4e-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