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LEMUR-2-DELOITTE-2

In orbit NORAD 68491 VEAQ-9641-6136-4817-6833

Falcon 9 Block 5

Carrier rocket

Space Launch Complex 4E

Spaceport

0

Observations all time

Mission information
Spacecraft name
LEMUR-2-DELOITTE-2
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
Separation time
Satellite appearance
Data for the last 30 days
Orbital parameters of the satellite
Perigee
584.76 km
Apogee
590.26 km
Inclination
97.8°
Period
96.5 min
Semi-major axis
6965.6 km
Velocity
7.57 km/s
Orbital elements
TLE source
Celestrak
TLE updated
2026-10-14 06:09:05 UTC
Two-line elements (TLE)
1 68491U 26067CD  26286.84887862  .00003167  00000-0  31490-3 0  9991
2 68491 97.7717 243.2398 0003947 39.5080 320.6426 14.92386947 29419
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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 04:26:23 LEMUR-2-DELOITTE-2
NORAD 68491
ISIS 1 DEB
NORAD 36301
2.557 15.48 2.3e-07
2026-10-16 23:27:11 IRIDE-MS2-HEO-5
NORAD 64571
LEMUR-2-DELOITTE-2
NORAD 68491
3.361 14.64 1.6e-07
2026-10-17 01:03:44 IRIDE-MS2-HEO-5
NORAD 64571
LEMUR-2-DELOITTE-2
NORAD 68491
1.383 14.64 9.4e-07
2026-10-17 02:40:18 IRIDE-MS2-HEO-5
NORAD 64571
LEMUR-2-DELOITTE-2
NORAD 68491
2.515 14.64 2.8e-07
2026-10-17 04:16:51 IRIDE-MS2-HEO-5
NORAD 64571
LEMUR-2-DELOITTE-2
NORAD 68491
4.956 14.64 7.3e-08
2026-10-17 05:05:08 IRIDE-MS2-HEO-5
NORAD 64571
LEMUR-2-DELOITTE-2
NORAD 68491
3.729 14.67 1.3e-07
2026-10-17 06:41:41 IRIDE-MS2-HEO-5
NORAD 64571
LEMUR-2-DELOITTE-2
NORAD 68491
3.903 14.67 1.2e-07
2026-10-17 12:29:32 LEMUR-2-DELOITTE-2
NORAD 68491
LEMUR-2-DELOITTE-5
NORAD 69910
3.454 7.22 3.3e-07
2026-10-19 01:48:20 LEMUR-2-DELOITTE-2
NORAD 68491
FENGYUN 1C DEB
NORAD 31608
4.955 14.96 6.5e-08
2026-10-20 02:24:39 LEMUR-2 FIKRETDENGIZ
NORAD 67363
LEMUR-2-DELOITTE-2
NORAD 68491
4.823 5.18 1.8e-07
2026-10-20 20:06:08 LEMUR-2-DELOITTE-2
NORAD 68491
COSMOS 2535
NORAD 44421
2.623 8.28 5.5e-07
2026-10-21 00:07:31 LEMUR-2-DELOITTE-2
NORAD 68491
COSMOS 2535
NORAD 44421
4.319 8.26 2.0e-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