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LEMUR-2-MARIO-SOUSA

In orbit NORAD 67365 YWIP-4605-7992-6916-2873

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-MARIO-SOUSA
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
590.75 km
Apogee
604.09 km
Inclination
97.8°
Period
96.7 min
Semi-major axis
6975.6 km
Velocity
7.55 km/s
Orbital elements
TLE source
Celestrak
TLE updated
2026-10-11 12:56:45 UTC
Two-line elements (TLE)
1 67365U 26004C   26283.97874732  .00003016  00000-0  32450-3 0  9994
2 67365  97.8063 280.8575 0009570 114.6230 245.5985 14.89211613 40520
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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 02:28:49 LEMUR-2-MARIO-SOUSA
NORAD 67365 		CSTB 1
NORAD 31122 		4.344 1.32 2.3e-07
2026-10-13 23:39:45 LEMUR-2-MARIO-SOUSA
NORAD 67365 		SL-14 R/B
NORAD 12849 		4.428 14.31 2.5e-07
2026-10-14 12:33:47 LEMUR-2-MARIO-SOUSA
NORAD 67365 		SL-14 R/B
NORAD 20466 		4.066 14.08 3.0e-07
2026-10-14 15:56:39 LEMUR-2-MARIO-SOUSA
NORAD 67365 		COSMOS 2251 DEB
NORAD 35614 		4.782 15.00 6.8e-08
2026-10-15 02:18:02 LEMUR-2-MARIO-SOUSA
NORAD 67365 		IRIDE-MS2-HEO-14
NORAD 68986 		4.047 11.63 1.9e-07
2026-10-15 20:02:11 LEMUR-2-MARIO-SOUSA
NORAD 67365 		GRUS-3B
NORAD 69918 		4.055 11.32 1.9e-07
2026-10-16 16:59:58 LEMUR-2-MARIO-SOUSA
NORAD 67365 		GRUS-3G
NORAD 69878 		3.434 11.32 2.7e-07
2026-10-17 09:00:44 LEMUR-2-MARIO-SOUSA
NORAD 67365 		CZ-4B DEB
NORAD 26207 		1.891 13.48 6.7e-07
2026-10-17 16:25:16 YAOGAN-2
NORAD 31490 		LEMUR-2-MARIO-SOUSA
NORAD 67365 		4.718 13.66 1.0e-07
2026-10-18 01:54:20 LEMUR-2-MARIO-SOUSA
NORAD 67365 		DELTA 1 DEB
NORAD 42567 		2.948 14.29 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