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Lemu Nge

In orbit NORAD 60532 KGKE-9945-4603-3909-1979 Chile

Falcon 9

Carrier rocket

База Вандерберг

Spaceport

0

Observations all time

Mission information
Spacecraft name
Lemu Nge
Other names
Forest Eye, Ojo del Bosque, Silvarum Oculus
Website
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
Spaceport
База Вандерберг
Launch time
2024-08-16 18:56:00
Separation time
2024-08-16 21:28:46
Satellite appearance
Data for the last 30 days
Orbital parameters of the satellite
Perigee
577.22 km
Apogee
579.58 km
Inclination
97.7°
Period
96.3 min
Semi-major axis
6956.5 km
Velocity
7.55 km/s
Orbital elements
TLE source
Celestrak
TLE updated
2026-10-10 12:56:49 UTC
Two-line elements (TLE)
1 60532U 24149BS  26283.16152983  .00001978  00000-0  18461-3 0  9990
2 60532 97.6748 355.7627 0001699 57.6811 302.4575 14.95317171117135
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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
2026-10-10 23:02:52 LEMU NGE
NORAD 60532
LEONAV-1
NORAD 69937
1.838 14.97 4.7e-07
2026-10-12 08:16:18 LEMU NGE
NORAD 60532
COSMOS 2251 DEB
NORAD 35587
3.218 15.07 1.5e-07
2026-10-12 14:44:59 LEMU NGE
NORAD 60532
FENGYUN 1C DEB
NORAD 31715
3.174 14.63 1.8e-07
2026-10-13 15:03:05 LEMU NGE
NORAD 60532
UNKNOWN
NORAD 82494
4.834 13.70 9.8e-08
2026-10-13 16:44:04 LEMU NGE
NORAD 60532
COSMOS 252 DEB
NORAD 9973
4.849 9.20 1.5e-07
2026-10-13 18:39:28 LEMU NGE
NORAD 60532
UVSQ-SAT NG
NORAD 63251
3.306 15.00 1.4e-07
2026-10-13 20:15:49 LEMU NGE
NORAD 60532
UVSQ-SAT NG
NORAD 63251
2.143 15.00 3.4e-07
2026-10-13 21:52:09 LEMU NGE
NORAD 60532
UVSQ-SAT NG
NORAD 63251
2.493 15.00 2.5e-07
2026-10-13 23:28:30 LEMU NGE
NORAD 60532
UVSQ-SAT NG
NORAD 63251
3.973 15.00 1.0e-07
2026-10-14 00:16:40 LEMU NGE
NORAD 60532
UVSQ-SAT NG
NORAD 63251
4.205 14.99 8.9e-08
2026-10-14 01:53:01 LEMU NGE
NORAD 60532
UVSQ-SAT NG
NORAD 63251
2.329 14.99 2.9e-07
2026-10-14 03:29:21 LEMU NGE
NORAD 60532
UVSQ-SAT NG
NORAD 63251
1.048 14.99 1.4e-06
2026-10-14 05:05:42 LEMU NGE
NORAD 60532
UVSQ-SAT NG
NORAD 63251
2.168 14.99 3.4e-07
2026-10-14 05:16:27 LATINSAT A
NORAD 27612
LEMU NGE
NORAD 60532
3.395 7.23 3.4e-07
2026-10-14 06:42:02 LEMU NGE
NORAD 60532
UVSQ-SAT NG
NORAD 63251
4.028 14.99 9.7e-08
2026-10-14 19:52:46 SOCRATES
NORAD 39768
LEMU NGE
NORAD 60532
4.422 5.36 2.1e-07
2026-10-14 21:29:08 SOCRATES
NORAD 39768
LEMU NGE
NORAD 60532
3.615 5.36 3.2e-07
2026-10-14 23:53:40 SOCRATES
NORAD 39768
LEMU NGE
NORAD 60532
4.464 5.37 2.1e-07
2026-10-15 14:39:09 LEMU NGE
NORAD 60532
DMSP 5D-2 F11 DEB
NORAD 28325
4.168 14.96 9.3e-08
2026-10-15 14:44:39 LEMU NGE
NORAD 60532
KUIPER-00551
NORAD 69618
3.892 14.60 1.2e-07
2026-10-15 21:18:57 LEMU NGE
NORAD 60532
CZ-2D R/B
NORAD 65853
3.911 13.09 1.7e-07
2026-10-15 21:37:13 LEMU NGE
NORAD 60532
DELTA 1 DEB
NORAD 26828
4.520 2.75 2.1e-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