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FLOCK 4BE-2

In orbit NORAD 60511 LLCH-7617-0470-2599-1004

Satellite appearance

Falcon 9 Block 5

Carrier rocket

Space Launch Complex 4E

Spaceport

0

Observations all time

Mission information
Spacecraft name
FLOCK 4BE-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
385.85 km
Apogee
391.15 km
Inclination
97.4°
Period
92.4 min
Semi-major axis
6766.6 km
Velocity
7.69 km/s
Orbital elements
TLE source
Celestrak
TLE updated
2026-08-05 12:36:58 UTC
Two-line elements (TLE)
1 60511U 24149AV  26216.24337849  .00082690  00000-0  10696-2 0  9999
2 60511 97.3804 305.1046 0003919 122.3603 237.8033 15.58641369109974
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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 12:48:35 STARLINK-11079
NORAD 58708
FLOCK 4BE-2
NORAD 60511
0.564 11.48 3.0e-04
2026-10-13 01:33:32 STARLINK-11609
NORAD 63132
FLOCK 4BE-2
NORAD 60511
4.200 7.04 6.8e-06
2026-10-13 05:33:09 STARLINK-11198
NORAD 60114
FLOCK 4BE-2
NORAD 60511
3.420 14.43 5.3e-06
2026-10-13 13:58:02 STARLINK-11478
NORAD 62557
FLOCK 4BE-2
NORAD 60511
3.132 12.63 8.6e-06
2026-10-13 14:32:23 STARLINK-11165
NORAD 60063
FLOCK 4BE-2
NORAD 60511
2.692 14.88 7.6e-06
2026-10-13 19:12:54 STARLINK-11131
NORAD 59756
FLOCK 4BE-2
NORAD 60511
3.513 14.81 4.5e-06
2026-10-13 19:24:59 SAMSAT-IONOSPHERE (RS75S)
NORAD 61784
FLOCK 4BE-2
NORAD 60511
4.072 14.66 1.2e-07
2026-10-13 22:52:36 STARLINK-11487
NORAD 62278
FLOCK 4BE-2
NORAD 60511
3.550 14.36 5.1e-06
2026-10-14 08:08:46 STARLINK-11711
NORAD 64378
FLOCK 4BE-2
NORAD 60511
0.469 14.47 2.8e-04
2026-10-14 12:31:17 STARLINK-11722
NORAD 64128
FLOCK 4BE-2
NORAD 60511
0.868 10.44 1.4e-04
2026-10-15 05:39:45 STARLINK-11405
NORAD 63008
FLOCK 4BE-2
NORAD 60511
0.749 9.99 1.9e-04
2026-10-15 09:32:00 STARLINK-11149
NORAD 60041
FLOCK 4BE-2
NORAD 60511
3.860 13.06 5.4e-06
2026-10-16 01:11:48 STARLINK-11636
NORAD 63194
FLOCK 4BE-2
NORAD 60511
3.361 8.87 9.9e-06
2026-10-16 03:43:01 STARLINK-11210
NORAD 60116
FLOCK 4BE-2
NORAD 60511
4.095 14.80 3.4e-06
2026-10-16 05:20:00 STARLINK-11685
NORAD 63552
FLOCK 4BE-2
NORAD 60511
4.889 12.90 3.4e-06
2026-10-16 07:37:17 STARLINK-11685
NORAD 63552
FLOCK 4BE-2
NORAD 60511
1.363 12.92 4.4e-05
2026-10-16 10:38:27 STARLINK-11497
NORAD 62470
FLOCK 4BE-2
NORAD 60511
2.087 8.79 2.6e-05
2026-10-16 14:16:57 STARLINK-38388
NORAD 100769
FLOCK 4BE-2
NORAD 60511
2.250 3.67 2.6e-05
2026-10-17 01:34:50 STARLINK-11570
NORAD 62992
FLOCK 4BE-2
NORAD 60511
0.352 11.08 7.9e-04
2026-10-17 03:41:32 STARLINK-37740
NORAD 100102
FLOCK 4BE-2
NORAD 60511
2.754 9.02 1.5e-05
2026-10-17 15:33:13 STARLINK-11585
NORAD 63309
FLOCK 4BE-2
NORAD 60511
4.002 7.27 7.5e-06

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