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FLOCK 4H 3

In orbit NORAD 66706 KJJR-9359-6972-6810-7679

Falcon 9 Block 5

Carrier rocket

Space Launch Complex 4E

Spaceport

5

Observations all time

Mission information
Spacecraft name
FLOCK 4H 3
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
497.42 km
Apogee
500.92 km
Inclination
97.4°
Period
94.7 min
Semi-major axis
6877.3 km
Velocity
7.61 km/s
Orbital elements
TLE source
Celestrak
TLE updated
2026-10-14 14:09:04 UTC
Two-line elements (TLE)
1 66706U 25276AS  26287.17752165  .00006810  00000-0  30832-3 0  9990
2 66706 97.4138 358.9807 0002544 319.9370 40.1678 15.21203952 48509
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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 18:12:01 OBJECT B
NORAD 63292
FLOCK 4H-3
NORAD 66706
3.349 8.61 3.3e-07
2026-10-17 06:51:13 BUZZER-1
NORAD 62609
FLOCK 4H-3
NORAD 66706
0.794 0.57 7.0e-06
2026-10-17 16:26:35 FLOCK 4H-3
NORAD 66706
USA 17
NORAD 16625
2.812 13.52 3.2e-07
2026-10-17 17:06:24 FLOCK 4H-3
NORAD 66706
ALSAT-3B
NORAD 67646
2.927 0.16 5.1e-07
2026-10-18 02:20:09 FLOCK 4H-3
NORAD 66706
HULIANWANG JISHU SHIYAN 9B
NORAD 68832
1.694 14.55 6.7e-07
2026-10-18 14:57:02 FLOCK 4H-3
NORAD 66706
HULIANWANG JISHU SHIYAN 10A
NORAD 69320
2.700 14.60 2.6e-07
2026-10-18 21:10:34 HERMES-1
NORAD 63242
FLOCK 4H-3
NORAD 66706
3.317 15.09 1.4e-07
2026-10-18 22:45:15 HERMES-1
NORAD 63242
FLOCK 4H-3
NORAD 66706
3.647 15.09 1.2e-07
2026-10-19 01:16:41 STARLINK-3264
NORAD 50198
FLOCK 4H-3
NORAD 66706
4.037 8.40 7.0e-06
2026-10-19 02:37:32 TOMORROW-S9
NORAD 66309
FLOCK 4H-3
NORAD 66706
0.490 14.41 8.3e-06
2026-10-19 06:35:32 CAS500-1
NORAD 47932
FLOCK 4H-3
NORAD 66706
4.670 15.09 7.2e-08
2026-10-19 08:54:45 SEMI-1N
NORAD 66297
FLOCK 4H-3
NORAD 66706
2.730 14.35 2.7e-07
2026-10-19 08:57:39 CAS500-1
NORAD 47932
FLOCK 4H-3
NORAD 66706
1.983 15.10 4.0e-07
2026-10-19 10:32:24 CAS500-1
NORAD 47932
FLOCK 4H-3
NORAD 66706
3.256 15.10 1.5e-07
2026-10-19 10:34:54 FLOCK 4H-3
NORAD 66706
IRIDIUM 33 DEB
NORAD 46971
1.900 15.22 4.1e-07
2026-10-19 13:03:25 HULIANWANG JISHU SHIYAN 6C
NORAD 63430
FLOCK 4H-3
NORAD 66706
3.084 14.58 2.0e-07
2026-10-19 20:56:26 HULIANWANG JISHU SHIYAN 6D
NORAD 63431
FLOCK 4H-3
NORAD 66706
3.251 14.61 1.8e-07
2026-10-19 21:12:39 LEO EXPRESS 2
NORAD 62673
FLOCK 4H-3
NORAD 66706
2.654 0.04 6.3e-07
2026-10-20 03:14:49 HULIANWANG JISHU SHIYAN 6B
NORAD 63429
FLOCK 4H-3
NORAD 66706
4.420 14.64 9.5e-08
2026-10-20 03:31:12 OTTER SDM
NORAD 66678
FLOCK 4H-3
NORAD 66706
4.030 0.04 2.7e-07
2026-10-20 04:18:44 OTTER SDM
NORAD 66678
FLOCK 4H-3
NORAD 66706
2.683 0.04 6.1e-07
2026-10-20 05:06:03 OTTER SDM
NORAD 66678
FLOCK 4H-3
NORAD 66706
1.867 0.04 1.3e-06
2026-10-20 05:53:11 OTTER SDM
NORAD 66678
FLOCK 4H-3
NORAD 66706
4.227 0.04 2.5e-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