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EMISAR

In orbit NORAD 68427 DOFN-8999-9141-5844-0576 Romania

Falcon 9 Block 5

Carrier rocket

Space Launch Complex 4E

Spaceport

37

Observations all time

Mission information
Spacecraft name
EMISAR
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
2026-03-30 11:02:00
Separation time
Last observers
Observer
Time of receipt
2026-06-20 11:27:47 UTC
2026-05-14 01:43:37 UTC
2026-04-22 10:44:29 UTC
2026-04-06 01:08:51 UTC
Satellite appearance
Data for the last 30 days
Orbital parameters of the satellite
Perigee
498.88 km
Apogee
500.06 km
Inclination
97.5°
Period
94.7 min
Semi-major axis
6877.6 km
Velocity
7.61 km/s
Orbital elements
TLE source
Celestrak
TLE updated
2026-10-14 06:09:05 UTC
Two-line elements (TLE)
1 68427U 26067M   26286.84755641  .00009643  00000-0  43641-3 0  9995
2 68427 97.4706 244.1320 0000862 52.4570 307.6744 15.21106798 29975
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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
2026-10-15 07:29:16 EMISAR
NORAD 68427
QUBE-II
NORAD 69023
4.219 7.73 2.2e-07
2026-10-15 15:13:57 SUPERVIEW NEO-1 04
NORAD 63126
EMISAR
NORAD 68427
2.364 14.73 3.2e-07
2026-10-15 16:48:40 SUPERVIEW NEO-1 04
NORAD 63126
EMISAR
NORAD 68427
2.115 14.73 4.0e-07
2026-10-15 17:36:01 SUPERVIEW NEO-1 04
NORAD 63126
EMISAR
NORAD 68427
3.906 14.70 1.2e-07
2026-10-15 18:23:23 SUPERVIEW NEO-1 04
NORAD 63126
EMISAR
NORAD 68427
4.887 14.73 7.6e-08
2026-10-15 19:10:44 SUPERVIEW NEO-1 04
NORAD 63126
EMISAR
NORAD 68427
1.211 14.70 1.2e-06
2026-10-15 20:45:27 SUPERVIEW NEO-1 04
NORAD 63126
EMISAR
NORAD 68427
2.847 14.70 2.2e-07
2026-10-16 09:21:53 STARLINK-5925
NORAD 55945
EMISAR
NORAD 68427
4.354 14.89 2.7e-06
2026-10-16 10:09:16 STARLINK-5925
NORAD 55945
EMISAR
NORAD 68427
4.925 14.92 2.1e-06
2026-10-16 19:01:12 STARLINK-4473
NORAD 53660
EMISAR
NORAD 68427
4.346 10.15 5.5e-06
2026-10-17 13:57:27 TRANSPORTER-13 OBJECT M
NORAD 63221
EMISAR
NORAD 68427
2.820 8.35 4.7e-07
2026-10-18 02:38:53 STARLINK-5500
NORAD 55634
EMISAR
NORAD 68427
4.664 12.81 3.7e-06
2026-10-18 11:49:49 STARLINK-5862
NORAD 55920
EMISAR
NORAD 68427
2.123 15.03 1.1e-05
2026-10-18 20:45:00 STARLINK-4472
NORAD 53661
EMISAR
NORAD 68427
4.759 10.18 4.6e-06
2026-10-19 02:14:52 TRANSPORTER-16 OBJECT L
NORAD 68426
EMISAR
NORAD 68427
3.298 0.02 4.0e-07
2026-10-19 12:27:42 TIANYI F
NORAD 64053
EMISAR
NORAD 68427
4.312 12.47 1.5e-07
2026-10-19 17:06:18 ION SCV-020
NORAD 64545
EMISAR
NORAD 68427
2.346 14.78 3.2e-07
2026-10-20 18:27:25 TIANYI D
NORAD 64051
EMISAR
NORAD 68427
4.306 12.45 1.5e-07
2026-10-20 23:05:43 CONNECTA IOT-12
NORAD 64553
EMISAR
NORAD 68427
3.522 14.81 1.4e-07
2026-10-21 00:40:25 CONNECTA IOT-12
NORAD 64553
EMISAR
NORAD 68427
1.290 14.81 1.1e-06
2026-10-21 02:15:08 CONNECTA IOT-12
NORAD 64553
EMISAR
NORAD 68427
1.076 14.81 1.5e-06
2026-10-21 03:49:50 CONNECTA IOT-12
NORAD 64553
EMISAR
NORAD 68427
3.300 14.81 1.6e-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