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LEMUR-2-DELOITTE-6

In orbit NORAD 69882 IHIJ-3887-7741-2822-7543

Observations 0
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Falcon 9 Block 5 | Transporter 17 (Dedicated SSO Rideshare)

Falcon 9 Block 5

Carrier rocket

Space Launch Complex 4E

Spaceport

0

Observations all time

Mission information
Spacecraft name
LEMUR-2-DELOITTE-6
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 | Transporter 17 (Dedicated SSO Rideshare)
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
588.44 km
Apogee
592.72 km
Inclination
97.7°
Period
96.6 min
Semi-major axis
6968.7 km
Velocity
7.55 km/s
Orbital elements
TLE source
Celestrak
TLE updated
2026-10-11 04:56:40 UTC
Two-line elements (TLE)
1 69882U 26156P   26283.95933472  .00001533  00000-0  15905-3 0  9991
2 69882  97.7467 182.7529 0003070 170.9252 189.2022 14.91402881 14259
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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
2026-10-11 10:39:28 TWILIGHT-1 OBJECT Z
NORAD 67386 		LEMUR-2-DELOITTE-6
NORAD 69882 		4.313 11.34 1.7e-07
2026-10-11 18:59:11 LEMUR-2-DELOITTE-6
NORAD 69882 		FENGYUN 1C DEB
NORAD 33678 		3.851 14.96 1.1e-07
2026-10-11 19:14:22 FFLY01
NORAD 65320 		LEMUR-2-DELOITTE-6
NORAD 69882 		4.440 14.96 8.0e-08
2026-10-12 00:21:20 LEMUR-2-DELOITTE-6
NORAD 69882 		SL-8 R/B
NORAD 12139 		1.437 11.16 7.6e-06
2026-10-12 07:38:07 LEMUR-2-DELOITTE-6
NORAD 69882 		SL-14 R/B
NORAD 16612 		3.451 14.77 3.4e-07
2026-10-13 07:05:12 YAM-10
NORAD 64580 		LEMUR-2-DELOITTE-6
NORAD 69882 		3.115 14.32 2.0e-07
2026-10-13 07:53:30 YAM-10
NORAD 64580 		LEMUR-2-DELOITTE-6
NORAD 69882 		1.503 14.35 8.7e-07
2026-10-13 09:42:47 LEMUR-2-DELOITTE-6
NORAD 69882 		CZ-6A DEB
NORAD 54576 		3.984 14.95 1.0e-07
2026-10-15 16:05:50 LEMUR-2-DELOITTE-6
NORAD 69882 		CZ-4C DEB
NORAD 42672 		4.066 11.53 1.9e-07
2026-10-16 07:32:42 BRITE-PL2 (HEWELIUSZ)
NORAD 40119 		LEMUR-2-DELOITTE-6
NORAD 69882 		2.881 14.28 2.4e-07
2026-10-17 00:08:05 O/OREOS (USA 219)
NORAD 37224 		LEMUR-2-DELOITTE-6
NORAD 69882 		4.374 4.58 2.2e-07
2026-10-17 00:26:05 LEMUR-2-DELOITTE-6
NORAD 69882 		SL-8 DEB
NORAD 5301 		1.972 14.70 4.5e-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