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

FLOCK 4H-10

In orbit NORAD 66713 RIFP-5026-4563-4732-6358

Observations 0
Go to map
Back

—

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-10
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
497.31 km
Apogee
501.51 km
Inclination
97.4°
Period
94.7 min
Semi-major axis
6877.5 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 66713U 25276AZ  26287.13639949  .00007526  00000-0  34112-3 0  9998
2 66713  97.4086 358.6703 0003056 321.0438  39.0577 15.21125149 48493
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
2026-10-15 11:21:25 FLOCK 4H-10
NORAD 66713 		COSMOS 2251 DEB
NORAD 33795 		4.839 14.97 7.1e-08
2026-10-15 14:27:02 FLOCK 4H-10
NORAD 66713 		IRIDE-MS1-EAGLET 2-15
NORAD 68462 		4.577 12.69 1.3e-07
2026-10-15 18:30:05 FLOCK 4H-10
NORAD 66713 		IRIDIUM 33 DEB
NORAD 46971 		0.627 15.18 3.8e-06
2026-10-15 21:55:37 FLOCK 4H-10
NORAD 66713 		COSMOS 249 DEB
NORAD 3757 		3.458 15.09 1.4e-07
2026-10-16 02:14:47 SKYKRAFT-1C
NORAD 55061 		FLOCK 4H-10
NORAD 66713 		3.635 2.69 3.3e-07
2026-10-16 06:57:13 FLOCK 4H-10
NORAD 66713 		CZ-4C DEB
NORAD 37569 		3.077 8.33 4.0e-07
2026-10-16 06:58:32 FLOCK 4H-10
NORAD 66713 		FLOCK 4H-36
NORAD 66739 		2.251 0.07 8.7e-07
2026-10-16 07:45:52 FLOCK 4H-10
NORAD 66713 		FLOCK 4H-36
NORAD 66739 		2.940 0.07 5.1e-07
2026-10-16 10:07:52 FLOCK 4H-10
NORAD 66713 		FLOCK 4H-22
NORAD 66725 		2.589 0.01 6.6e-07
2026-10-16 10:52:18 FLOCK 4H-10
NORAD 66713 		FLOCK 4H-22
NORAD 66725 		4.222 0.01 2.4e-07
2026-10-17 12:58:24 FLOCK 4H-9
NORAD 66712 		FLOCK 4H-10
NORAD 66713 		2.441 0.06 7.4e-07
2026-10-17 13:45:38 FLOCK 4H-9
NORAD 66712 		FLOCK 4H-10
NORAD 66713 		3.453 0.06 3.7e-07
2026-10-18 00:02:32 FLOCK 4H-10
NORAD 66713 		RASSVET-3 18
NORAD 100084 		4.113 13.83 1.3e-07
2026-10-18 07:45:16 STARLINK-4624
NORAD 53684 		FLOCK 4H-10
NORAD 66713 		4.848 14.87 2.2e-06
2026-10-18 20:46:41 KANOPUS-V 3
NORAD 43180 		FLOCK 4H-10
NORAD 66713 		0.730 15.01 3.0e-06
2026-10-19 06:01:39 ITASAT
NORAD 43786 		FLOCK 4H-10
NORAD 66713 		4.230 2.93 2.4e-07
2026-10-19 06:22:26 FGN-100-D2
NORAD 66299 		FLOCK 4H-10
NORAD 66713 		1.087 14.40 1.7e-06
2026-10-19 13:08:47 PAZ
NORAD 43215 		FLOCK 4H-10
NORAD 66713 		3.310 8.20 3.5e-07
2026-10-19 15:29:03 SCS-01 L
NORAD 63992 		FLOCK 4H-10
NORAD 66713 		2.723 0.18 6.0e-07
2026-10-19 17:51:07 SCS-01 L
NORAD 63992 		FLOCK 4H-10
NORAD 66713 		3.046 0.18 4.8e-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