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LEMUR-2 FIKRETDENGIZ

In orbit NORAD 67363 ZNER-8524-4467-2780-2301

Observations 0
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Falcon 9 Block 5 | Pandora / Twilight rideshare mission

Falcon 9 Block 5

Carrier rocket

Space Launch Complex 4E

Spaceport

0

Observations all time

Mission information
Spacecraft name
LEMUR-2 FIKRETDENGIZ
Status
Active
The satellite is in orbit
The network has not received data from this satellite for a long time
Launch and timeline
Launch
Falcon 9 Block 5 | Pandora / Twilight rideshare mission
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
590.96 km
Apogee
605.01 km
Inclination
97.8°
Period
96.7 min
Semi-major axis
6976.1 km
Velocity
7.56 km/s
Orbital elements
TLE source
Celestrak
TLE updated
2026-10-11 12:56:45 UTC
Two-line elements (TLE)
1 67363U 26004A   26284.21311231  .00004425  00000-0  47533-3 0  9993
2 67363  97.8095 281.1002 0010079 113.3692 246.8587 14.89032565 40547
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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
2026-10-12 12:24:19 LEMUR-2 FIKRETDENGIZ
NORAD 67363 		CZ-2C R/B
NORAD 48862 		1.865 11.00 9.2e-07
2026-10-13 10:24:50 LEMUR-2 FIKRETDENGIZ
NORAD 67363 		FENGYUN 1C DEB
NORAD 30569 		3.859 14.95 1.1e-07
2026-10-13 12:01:38 LEMUR-2 FIKRETDENGIZ
NORAD 67363 		FENGYUN 1C DEB
NORAD 30569 		1.339 14.95 8.9e-07
2026-10-15 02:26:32 KAZEOSAT 2
NORAD 40010 		LEMUR-2 FIKRETDENGIZ
NORAD 67363 		2.959 14.80 1.9e-07
2026-10-15 20:50:10 LEMUR-2 FIKRETDENGIZ
NORAD 67363 		SPEAR-1A
NORAD 69900 		2.773 11.32 4.1e-07
2026-10-16 13:39:22 BRITE-CA1 (TORONTO)
NORAD 40020 		LEMUR-2 FIKRETDENGIZ
NORAD 67363 		2.192 13.56 4.9e-07
2026-10-17 03:23:02 IRIDE-MS2-HEO-5
NORAD 64571 		LEMUR-2 FIKRETDENGIZ
NORAD 67363 		2.805 12.70 3.4e-07
2026-10-17 07:57:52 LEMUR-2 FIKRETDENGIZ
NORAD 67363 		DELTA 1 DEB
NORAD 10220 		2.518 13.21 4.0e-07
2026-10-17 13:09:15 LEMUR-2 FIKRETDENGIZ
NORAD 67363 		FOSSASAT-2E26
NORAD 69899 		3.143 11.33 3.2e-07
2026-10-17 20:03:09 LEMUR-2 FIKRETDENGIZ
NORAD 67363 		DELTA 2 R/B(1)
NORAD 22276 		3.193 12.05 1.4e-06
2026-10-17 21:13:03 LEMUR-2 FIKRETDENGIZ
NORAD 67363 		LEMUR-2-ALEX-FULTON
NORAD 69905 		4.733 11.33 1.4e-07
2026-10-17 22:44:37 LEMUR-2 FIKRETDENGIZ
NORAD 67363 		CZ-6A DEB
NORAD 61145 		4.934 5.37 1.7e-07
2026-10-18 00:15:20 LEMUR-2 FIKRETDENGIZ
NORAD 67363 		NOAA 16 DEB
NORAD 41348 		4.956 14.62 7.4e-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