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OPTISAT

In orbit NORAD 68418 EDMF-5886-6201-4785-7103 Greece

Time in UTC

15.10 10:28

Scheduled · Сампо-400 [R1NAV]

111

Observations over 30 days

83%

Successful observations

40k

Frames, latest 2026-10-15 01:22 UTC

Launch and timeline
Carrier rocket
Falcon 9 Block 5
Spaceport
Space Launch Complex 4E
Launch time
2025-03-30 13:20:00
Separation time
Last observers
Observer
Time of receipt
2026-10-15 01:22:32 UTC
2026-10-14 12:28:41 UTC
2026-10-14 10:54:11 UTC
2026-10-14 01:37:38 UTC
2026-10-13 12:46:41 UTC
Satellite appearance
Data for the last 30 days
Orbital parameters of the satellite
Perigee
502.46 km
Apogee
503.96 km
Inclination
97.5°
Period
94.7 min
Semi-major axis
6881.3 km
Velocity
7.61 km/s
Orbital elements
TLE source
Celestrak
TLE updated
2026-10-14 14:09:05 UTC
Two-line elements (TLE)
1 68418U 26067C   26287.11087402  .00004076  00000-0  19321-3 0  9992
2 68418 97.4747 244.3389 0001086 182.7857 177.3372 15.19867603 30002
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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
2026-10-16 13:28:02 ZIYUAN 3-02 (ZY 3-02)
NORAD 41556
OPTISAT
NORAD 68418
1.733 12.81 8.9e-07
2026-10-17 11:33:19 STARLINK-6061
NORAD 56795
OPTISAT
NORAD 68418
2.308 13.47 1.4e-05
2026-10-17 18:44:15 CONNECTA IOT-15
NORAD 67402
OPTISAT
NORAD 68418
2.902 5.15 5.0e-07
2026-10-17 20:55:55 STARLINK-5925
NORAD 55945
OPTISAT
NORAD 68418
3.710 15.01 3.6e-06
2026-10-19 02:49:33 RASSVET-3 2
NORAD 68361
OPTISAT
NORAD 68418
3.717 2.11 3.2e-07
2026-10-19 07:49:49 OBJECT AK
NORAD 67281
OPTISAT
NORAD 68418
3.917 12.75 1.8e-07
2026-10-19 17:53:27 STARLINK-5862
NORAD 55920
OPTISAT
NORAD 68418
2.656 15.08 6.7e-06
2026-10-19 18:08:57 OPTISAT
NORAD 68418
DB GME UT (DB-GLOBE MISSION EARTH-UT)
NORAD 68459
4.870 0.08 1.9e-07
2026-10-19 18:40:51 STARLINK-5862
NORAD 55920
OPTISAT
NORAD 68418
3.516 15.10 3.8e-06
2026-10-19 18:56:18 OPTISAT
NORAD 68418
DB GME UT (DB-GLOBE MISSION EARTH-UT)
NORAD 68459
3.329 0.08 4.0e-07
2026-10-20 02:49:15 OPTISAT
NORAD 68418
RASSVET-3 32
NORAD 100098
3.299 13.17 2.3e-07
2026-10-20 19:22:52 LYRA-1
NORAD 62664
OPTISAT
NORAD 68418
4.368 12.69 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