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

FLOCK 4H-18

In orbit NORAD 66721 OVJF-2979-4927-0624-6119

Falcon 9 Block 5

Carrier rocket

Space Launch Complex 4E

Spaceport

0

Observations all time

Mission information
Spacecraft name
FLOCK 4H-18
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
497.41 km
Apogee
502.08 km
Inclination
97.4°
Period
94.7 min
Semi-major axis
6877.9 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 66721U 25276BH  26284.19270673  .00008155  00000-0  37051-3 0  9999
2 66721 97.4082 355.6794 0003380 6.5082 353.6197 15.21016915 48049
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
2026-10-12 07:14:32 FLOCK 4H-18
NORAD 66721
COSMOS 2251 DEB
NORAD 34128
4.911 4.87 1.7e-07
2026-10-12 17:20:52 SHIJIAN-6 01A (SJ-6 01A)
NORAD 28413
FLOCK 4H-18
NORAD 66721
1.125 5.65 3.3e-06
2026-10-12 20:32:29 FLOCK 4H-18
NORAD 66721
IRIDE-MS1-EAGLET 2-9
NORAD 68449
3.212 12.71 2.6e-07
2026-10-13 15:29:17 FLOCK 4H-18
NORAD 66721
COSMO
NORAD 68460
1.292 12.71 1.6e-06
2026-10-14 05:53:08 STARLINK-1451
NORAD 45668
FLOCK 4H-18
NORAD 66721
4.245 14.38 3.4e-06
2026-10-14 09:35:28 FLOCK 4H-18
NORAD 66721
ZIYUAN 3-04 (ZY 3-04)
NORAD 67131
4.633 0.73 2.1e-07
2026-10-14 11:57:33 FLOCK 4H-18
NORAD 66721
ZIYUAN 3-04 (ZY 3-04)
NORAD 67131
3.842 0.73 3.0e-07
2026-10-14 13:09:50 ETIHAD-SAT
NORAD 63226
FLOCK 4H-18
NORAD 66721
2.619 15.10 2.3e-07
2026-10-14 22:47:21 FLOCK 4H-18
NORAD 66721
OBJECT H
NORAD 51953
4.262 5.66 2.3e-07
2026-10-15 01:17:31 KOYOH
NORAD 58464
FLOCK 4H-18
NORAD 66721
2.088 0.04 1.0e-06
2026-10-15 04:35:28 FLOCK 4H-18
NORAD 66721
VIGORIDE-7
NORAD 68473
4.869 12.60 1.2e-07
2026-10-15 20:19:45 FLOCK 4H-18
NORAD 66721
FLOCK 4H-25
NORAD 66728
3.820 0.07 3.0e-07
2026-10-15 20:45:31 ORBASTRO-TR5
NORAD 63236
FLOCK 4H-18
NORAD 66721
3.797 15.10 1.1e-07
2026-10-15 21:55:42 FLOCK 4H-18
NORAD 66721
IRIDIUM 33 DEB
NORAD 40996
2.705 14.51 2.6e-07
2026-10-15 22:40:36 BLACKJACK ACES-1
NORAD 56956
FLOCK 4H-18
NORAD 66721
4.482 8.08 1.9e-07
2026-10-16 16:12:11 IRIDE-MS1-EAGLET 2-4
NORAD 66698
FLOCK 4H-18
NORAD 66721
3.905 0.01 2.9e-07
2026-10-16 16:46:44 IRIDE-MS1-EAGLET 2-4
NORAD 66698
FLOCK 4H-18
NORAD 66721
4.176 0.01 2.9e-07
2026-10-16 17:35:36 IRIDE-MS1-EAGLET 2-4
NORAD 66698
FLOCK 4H-18
NORAD 66721
2.062 0.00 1.3e-06
2026-10-16 18:26:52 IRIDE-MS1-EAGLET 2-4
NORAD 66698
FLOCK 4H-18
NORAD 66721
1.816 0.01 1.3e-06
2026-10-17 01:30:37 FLOCK 4H-18
NORAD 66721
CZ-6A DEB
NORAD 56246
4.010 8.50 2.3e-07
2026-10-17 14:09:23 FOSSASAT-2E21
NORAD 64536
FLOCK 4H-18
NORAD 66721
2.661 5.38 5.9e-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