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Marina

In orbit NORAD 69920 FZQD-0263-2257-6241-5637 Slovakia

Time in UTC

20:20

Next pass · Чукотка · 41°

11.10 22:23

Scheduled · Сампо-435 [R1NAV]

102

Observations over 30 days

82%

Successful observations

67k

Frames, latest 2026-10-10 07:30 UTC

Mission information
Spacecraft name
Marina
Call sign
OM9MAR
Status
Active
The satellite is in orbit
Launch and timeline
Carrier rocket
Falcon 9
Spaceport
База Вандерберг
Launch time
2026-07-07 07:12:00
Separation time
2026-07-07 08:00:16
Last observers
Observer
Time of receipt
2026-10-10 07:30:06 UTC
2026-10-10 07:28:37 UTC
2026-10-09 22:07:33 UTC
2026-10-09 20:31:47 UTC
2026-10-09 07:21:52 UTC
Satellite appearance
Data for the last 30 days
Orbital parameters of the satellite
Perigee
583.20 km
Apogee
592.73 km
Inclination
97.7°
Period
96.5 min
Semi-major axis
6966.1 km
Velocity
7.55 km/s
Orbital elements
TLE source
Celestrak
TLE updated
2026-10-10 04:46:21 UTC
Two-line elements (TLE)
1 69920U 26156BD  26282.96587758  .00001710  00000-0  17314-3 0  9999
2 69920 97.7424 181.8517 0006846 188.8543 171.2557 14.92241736 14117
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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 21:16:01 MARINA
NORAD 69920
CZ-2D DEB
NORAD 44612
0.749 11.57 5.4e-06
2026-10-11 02:14:36 BRITE-PL2 (HEWELIUSZ)
NORAD 40119
MARINA
NORAD 69920
2.513 14.29 3.1e-07
2026-10-11 11:05:33 HUBBLE 7
NORAD 64592
MARINA
NORAD 69920
3.167 14.32 2.0e-07
2026-10-11 18:56:41 MARINA
NORAD 69920
FENGYUN 1C DEB
NORAD 29833
3.640 13.86 1.7e-07
2026-10-12 20:02:50 MARINA
NORAD 69920
COSMOS 921
NORAD 10095
2.911 14.62 2.1e-07
2026-10-14 00:12:13 MARINA
NORAD 69920
HORYU-2
NORAD 38340
1.302 13.03 1.5e-06
2026-10-14 02:37:03 MARINA
NORAD 69920
HORYU-2
NORAD 38340
4.767 13.00 1.1e-07
2026-10-14 10:14:58 BRO-31
NORAD 69896
MARINA
NORAD 69920
4.778 0.01 1.9e-07
2026-10-14 11:52:39 BRO-31
NORAD 69896
MARINA
NORAD 69920
3.392 0.00 1.9e-05
2026-10-14 13:34:46 BRO-31
NORAD 69896
MARINA
NORAD 69920
2.037 0.00 1.9e-05
2026-10-14 14:47:04 BRO-31
NORAD 69896
MARINA
NORAD 69920
0.947 0.00 1.9e-05
2026-10-14 15:20:53 BRO-31
NORAD 69896
MARINA
NORAD 69920
0.701 0.00 1.9e-05
2026-10-14 16:10:30 BRO-31
NORAD 69896
MARINA
NORAD 69920
0.469 0.00 1.9e-05
2026-10-14 17:04:02 BRO-31
NORAD 69896
MARINA
NORAD 69920
0.676 0.00 1.9e-05
2026-10-14 18:44:14 BRO-31
NORAD 69896
MARINA
NORAD 69920
2.064 0.00 1.9e-05
2026-10-14 20:22:32 BRO-31
NORAD 69896
MARINA
NORAD 69920
3.472 0.00 1.9e-05
2026-10-14 21:59:58 BRO-31
NORAD 69896
MARINA
NORAD 69920
4.890 0.01 1.8e-07
2026-10-15 04:52:32 ARCTIC WEATHER SATELLITE
NORAD 60543
MARINA
NORAD 69920
3.434 14.91 1.4e-07
2026-10-15 06:12:12 MARINA
NORAD 69920
COSMOS 2251 DEB
NORAD 37968
1.841 15.03 4.5e-07
2026-10-15 08:13:45 MARINA
NORAD 69920
THOR ABLESTAR DEB
NORAD 15783
3.720 13.10 1.8e-07
2026-10-15 23:15:03 CONNECTA IOT-7
NORAD 62715
MARINA
NORAD 69920
4.375 14.99 8.2e-08
2026-10-16 00:51:32 CONNECTA IOT-7
NORAD 62715
MARINA
NORAD 69920
4.964 14.99 6.4e-08

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