RU | EN | ZH --:-- UTC Sign in

LEMUR-2-ALEX-FULTON

In orbit NORAD 69905 KTJQ-9520-5233-8125-7671

Falcon 9 Block 5

Carrier rocket

Space Launch Complex 4E

Spaceport

0

Observations all time

Mission information
Spacecraft name
LEMUR-2-ALEX-FULTON
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
588.01 km
Apogee
592.58 km
Inclination
97.7°
Period
96.5 min
Semi-major axis
6968.4 km
Velocity
7.56 km/s
Orbital elements
TLE source
Celestrak
TLE updated
2026-10-10 04:46:21 UTC
Two-line elements (TLE)
1 69905U 26156AN  26282.95277717  .00003943  00000-0  39936-3 0  9996
2 69905 97.7473 181.7691 0003280 158.2265 201.9094 14.91494947 14106
Copy content
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 23:31:33 RCM-2
NORAD 44324
LEMUR-2-ALEX-FULTON
NORAD 69905
3.904 12.06 1.9e-07
2026-10-12 03:16:58 FFLY01
NORAD 65320
LEMUR-2-ALEX-FULTON
NORAD 69905
4.027 14.96 9.8e-08
2026-10-12 12:51:49 LEMUR-2-ALEX-FULTON
NORAD 69905
DELTA 1 DEB
NORAD 10471
3.744 13.78 1.7e-07
2026-10-12 22:15:19 PROPCUBE 3
NORAD 40973
LEMUR-2-ALEX-FULTON
NORAD 69905
2.554 8.33 5.8e-07
2026-10-13 16:38:30 LEMUR-2-ALEX-FULTON
NORAD 69905
REPLICATOR 2
NORAD 69927
4.371 0.02 2.3e-07
2026-10-13 17:26:19 LEMUR-2-ALEX-FULTON
NORAD 69905
REPLICATOR 2
NORAD 69927
1.107 0.02 3.6e-06
2026-10-14 07:13:43 YAM-10
NORAD 64580
LEMUR-2-ALEX-FULTON
NORAD 69905
4.630 14.32 9.2e-08
2026-10-14 08:02:01 YAM-10
NORAD 64580
LEMUR-2-ALEX-FULTON
NORAD 69905
4.367 14.35 1.0e-07
2026-10-14 08:50:18 YAM-10
NORAD 64580
LEMUR-2-ALEX-FULTON
NORAD 69905
4.094 14.32 1.2e-07
2026-10-14 09:38:36 YAM-10
NORAD 64580
LEMUR-2-ALEX-FULTON
NORAD 69905
0.941 14.35 2.2e-06
2026-10-15 12:04:57 LEMUR-2-CARROLLEMO
NORAD 68489
LEMUR-2-ALEX-FULTON
NORAD 69905
2.016 7.20 9.7e-07
2026-10-15 16:12:10 HYPERION GR-1
NORAD 69883
LEMUR-2-ALEX-FULTON
NORAD 69905
4.083 0.01 2.6e-07
2026-10-15 17:33:25 HYPERION GR-1
NORAD 69883
LEMUR-2-ALEX-FULTON
NORAD 69905
4.131 0.00 2.4e-07
2026-10-15 18:30:08 HYPERION GR-1
NORAD 69883
LEMUR-2-ALEX-FULTON
NORAD 69905
2.974 0.01 5.0e-07
2026-10-15 21:01:18 LEMUR-2-ALEX-FULTON
NORAD 69905
IRIDIUM 33 DEB
NORAD 34079
2.403 5.38 7.2e-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