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Zorkiy-2M 7

In orbit NORAD 67268 IGYJ-8963-1038-8735-2733 Спутникс Russia

Time in UTC

21:13

Next pass · Тверь

—

No observations scheduled

2

Observations over 30 days

78%

Successful observations

43

Frames, latest 2026-09-18 08:06 UTC

Mission information
Spacecraft name
Zorkiy-2M 7
Other names
A0XAA, A0XAB
Call sign
A0XAA
Status
Active
The satellite is in orbit
Launch and timeline
Carrier rocket
Soyuz 2.1b Fregat-M
Upper stage
Фрегат-М
Spaceport
Cosmodrome Site 1S
Launch time
2025-12-28 13:18:05
Separation time
Last observers
Observer
Time of receipt
2026-09-18 08:06:47 UTC
2026-09-13 08:19:35 UTC
2026-05-02 08:45:58 UTC
2026-04-28 19:17:53 UTC
2026-04-23 19:25:24 UTC
Satellite appearance
Operator
Data for the last 30 days
Orbital parameters of the satellite
Perigee
482.03 km
Apogee
500.27 km
Inclination
97.4°
Period
94.5 min
Semi-major axis
6869.2 km
Velocity
7.62 km/s
Orbital elements
TLE source
Celestrak
TLE updated
2026-10-12 13:08:42 UTC
Two-line elements (TLE)
1 67268U 25313W   26285.15333143  .00008049  00000-0  33555-3 0  9994
2 67268 97.3849 357.9531 0013160 317.4229 42.5987 15.23882483 43751
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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 19:31:21 ZORKY-2M 7
NORAD 67268
AISSAT 4
NORAD 68454
4.895 12.79 1.1e-07
2026-10-14 00:46:30 AEROCUBE 8D
NORAD 41852
ZORKY-2M 7
NORAD 67268
3.903 14.97 1.1e-07
2026-10-14 03:41:53 ZORKY-2M 7
NORAD 67268
GEN1A-1
NORAD 69004
0.803 15.09 2.4e-06
2026-10-14 15:24:42 STARLINK-6190
NORAD 56774
ZORKY-2M 7
NORAD 67268
3.937 15.09 3.1e-06
2026-10-14 20:44:12 ZORKY-2M 7
NORAD 67268
IRIDE-MS1-EAGLET 2-13
NORAD 68450
3.336 12.78 2.4e-07
2026-10-15 04:08:19 YAOGAN-35 03B
NORAD 53318
ZORKY-2M 7
NORAD 67268
3.955 13.91 1.4e-07
2026-10-15 10:52:02 TRANSPORTER-12 OBJECT BR
NORAD 62672
ZORKY-2M 7
NORAD 67268
4.722 0.60 2.0e-07
2026-10-15 13:34:29 ZORKY-2M 7
NORAD 67268
EDDA-1
NORAD 69017
2.290 15.11 3.0e-07
2026-10-16 00:15:04 FORGESTAR-1
NORAD 64546
ZORKY-2M 7
NORAD 67268
4.253 5.51 2.3e-07
2026-10-16 12:51:28 T1DES 1 (DRAGOON 1)
NORAD 64542
ZORKY-2M 7
NORAD 67268
3.107 5.60 4.3e-07
2026-10-16 18:43:13 ZORKY-2M 7
NORAD 67268
JACKAL-004
NORAD 69012
3.777 15.09 1.1e-07
2026-10-16 20:46:01 ZORKY-2M 7
NORAD 67268
RASSVET-3 20
NORAD 100086
2.252 13.87 4.5e-07
2026-10-17 04:47:06 STARLINK-5265
NORAD 55317
ZORKY-2M 7
NORAD 67268
3.828 14.92 3.5e-06
2026-10-17 06:21:36 STARLINK-5265
NORAD 55317
ZORKY-2M 7
NORAD 67268
4.110 14.92 3.0e-06
2026-10-17 14:38:18 STARLINK-4636
NORAD 53731
ZORKY-2M 7
NORAD 67268
2.172 7.28 2.5e-05
2026-10-17 17:15:13 ZORKY-2M 7
NORAD 67268
RASSVET-3 28
NORAD 100094
4.392 13.77 1.2e-07
2026-10-18 01:54:52 FLOCK 4H-34
NORAD 66737
ZORKY-2M 7
NORAD 67268
4.757 0.09 1.9e-07
2026-10-18 05:24:05 ZORKY-2M 7
NORAD 67268
BALKAN-2
NORAD 69024
4.641 15.09 7.3e-08
2026-10-18 10:10:04 ZORKY-2M 7
NORAD 67268
IRIDIUM 33 DEB
NORAD 46971
3.876 15.22 9.8e-08
2026-10-18 17:41:06 HAWK-12C
NORAD 64621
ZORKY-2M 7
NORAD 67268
3.992 8.90 2.3e-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