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FLOCK 4H-25

In orbit NORAD 66728 MXAM-8049-0304-5884-9193

Falcon 9 Block 5

Carrier rocket

Space Launch Complex 4E

Spaceport

0

Observations all time

Mission information
Spacecraft name
FLOCK 4H-25
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
496.54 km
Apogee
498.10 km
Inclination
97.4°
Period
94.6 min
Semi-major axis
6875.4 km
Velocity
7.6 km/s
Orbital elements
TLE source
Celestrak
TLE updated
2026-10-11 12:56:45 UTC
Two-line elements (TLE)
1 66728U 25276BQ  26284.19518709  .00008180  00000-0  36291-3 0  9994
2 66728 97.4097 356.1949 0001152 123.5433 236.5913 15.21833910 47355
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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 07:32:10 ETIHAD-SAT
NORAD 63226
FLOCK 4H-25
NORAD 66728
4.191 15.10 8.9e-08
2026-10-12 09:06:49 ETIHAD-SAT
NORAD 63226
FLOCK 4H-25
NORAD 66728
4.113 15.10 9.3e-08
2026-10-12 11:28:49 ETIHAD-SAT
NORAD 63226
FLOCK 4H-25
NORAD 66728
3.962 15.10 1.0e-07
2026-10-12 13:03:28 ETIHAD-SAT
NORAD 63226
FLOCK 4H-25
NORAD 66728
2.404 15.10 2.7e-07
2026-10-12 14:38:07 ETIHAD-SAT
NORAD 63226
FLOCK 4H-25
NORAD 66728
4.777 15.10 6.9e-08
2026-10-13 04:50:13 SPACEEYE-T1
NORAD 63229
FLOCK 4H-25
NORAD 66728
3.921 15.10 1.0e-07
2026-10-13 12:21:36 FLOCK 4H-25
NORAD 66728
TRANSPORTER-16 OBJECT AT
NORAD 68457
1.456 12.71 1.3e-06
2026-10-13 13:08:57 FLOCK 4H-25
NORAD 66728
TRANSPORTER-16 OBJECT AT
NORAD 68457
1.961 12.68 7.1e-07
2026-10-13 14:03:44 SPACEMOBILE-001
NORAD 61047
FLOCK 4H-25
NORAD 66728
2.597 13.39 3.7e-07
2026-10-14 13:47:14 STARLINK-1451
NORAD 45668
FLOCK 4H-25
NORAD 66728
4.626 14.32 2.9e-06
2026-10-14 14:34:36 STARLINK-1451
NORAD 45668
FLOCK 4H-25
NORAD 66728
4.100 14.30 3.7e-06
2026-10-14 19:31:08 ORBASTRO-TR5
NORAD 63236
FLOCK 4H-25
NORAD 66728
3.912 15.10 1.0e-07
2026-10-14 23:27:47 ORBASTRO-TR5
NORAD 63236
FLOCK 4H-25
NORAD 66728
2.663 15.09 2.2e-07
2026-10-15 01:02:25 ORBASTRO-TR5
NORAD 63236
FLOCK 4H-25
NORAD 66728
4.114 15.09 9.3e-08
2026-10-15 06:08:47 FLOCK 4H-25
NORAD 66728
IRIDIUM 33 DEB
NORAD 40996
2.049 14.50 4.6e-07
2026-10-15 14:01:02 FLOCK 4H-25
NORAD 66728
FLOCK 4H-29
NORAD 66732
2.366 0.07 7.9e-07
2026-10-15 14:48:18 FLOCK 4H-25
NORAD 66728
FLOCK 4H-29
NORAD 66732
3.897 0.07 2.9e-07
2026-10-15 23:29:08 FLOCK 4H-18
NORAD 66721
FLOCK 4H-25
NORAD 66728
3.086 0.07 4.6e-07
2026-10-16 00:16:28 FLOCK 4H-18
NORAD 66721
FLOCK 4H-25
NORAD 66728
3.989 0.07 2.8e-07
2026-10-16 07:33:51 STARLINK-5296
NORAD 55312
FLOCK 4H-25
NORAD 66728
2.950 15.00 5.6e-06
2026-10-17 00:43:58 FLOCK 4H-25
NORAD 66728
MERCURY ONE (M1)
NORAD 66742
3.783 0.06 3.1e-07
2026-10-17 06:00:55 YAOGAN-39 03C
NORAD 57990
FLOCK 4H-25
NORAD 66728
4.600 12.13 1.4e-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