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FLOCK 4H-32

In orbit NORAD 66735 EBEB-6786-0977-5359-4600

Observations 0
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Falcon 9 Block 5 | Transporter 15 (Dedicated SSO Rideshare)

Falcon 9 Block 5

Carrier rocket

Space Launch Complex 4E

Spaceport

0

Observations all time

Mission information
Spacecraft name
FLOCK 4H-32
Status
Active
The satellite is in orbit
The network has not received data from this satellite for a long time
Launch and timeline
Launch
Falcon 9 Block 5 | Transporter 15 (Dedicated SSO Rideshare)
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
497.46 km
Apogee
502.36 km
Inclination
97.4°
Period
94.7 min
Semi-major axis
6878.0 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 66735U 25276BX  26284.19321933  .00007853  00000-0  35749-3 0  9996
2 66735  97.4129 355.8720 0003546 340.4618  19.6481 15.20961670 48047
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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 06:16:16 OBJECT B
NORAD 63292 		FLOCK 4H-32
NORAD 66735 		4.402 8.61 1.9e-07
2026-10-12 14:18:34 FLOCK 4H-32
NORAD 66735 		JD 1
NORAD 14728 		2.954 10.65 3.9e-07
2026-10-12 14:58:52 FLOCK 4H-14
NORAD 66717 		FLOCK 4H-32
NORAD 66735 		3.740 0.07 3.2e-07
2026-10-13 19:48:49 ETIHAD-SAT
NORAD 63226 		FLOCK 4H-32
NORAD 66735 		4.130 15.10 9.2e-08
2026-10-14 16:45:56 FLOCK 4H-32
NORAD 66735 		COSMO
NORAD 68460 		2.286 12.73 5.2e-07
2026-10-14 20:42:44 FLOCK 4H-32
NORAD 66735 		VIGORIDE-7
NORAD 68473 		4.936 12.61 1.1e-07
2026-10-15 10:53:31 FLOCK 4H-32
NORAD 66735 		IRIDIUM 33 DEB
NORAD 40996 		2.397 14.49 3.4e-07
2026-10-15 15:24:51 KOYOH
NORAD 58464 		FLOCK 4H-32
NORAD 66735 		3.491 0.02 3.6e-07
2026-10-15 21:58:32 FLOCK 4H-32
NORAD 66735 		TRANSPORTER-16 OBJECT AT
NORAD 68457 		3.758 12.66 1.9e-07
2026-10-15 23:33:15 FLOCK 4H-32
NORAD 66735 		TRANSPORTER-16 OBJECT AT
NORAD 68457 		3.161 12.66 2.7e-07
2026-10-16 00:20:36 FLOCK 4H-32
NORAD 66735 		TRANSPORTER-16 OBJECT AT
NORAD 68457 		4.083 12.68 1.6e-07
2026-10-16 05:48:25 BRO-18
NORAD 64550 		FLOCK 4H-32
NORAD 66735 		4.257 5.48 2.3e-07
2026-10-16 21:50:20 KANOPUS-V-IK
NORAD 42825 		FLOCK 4H-32
NORAD 66735 		1.371 15.01 8.6e-07
2026-10-17 07:05:23 FLOCK 4H-32
NORAD 66735 		OBJECT D
NORAD 67251 		3.990 0.86 2.8e-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