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

FLOCK 4BE-19

In orbit NORAD 60563 GOTO-5562-2042-5828-2742

Observations 0
Go to map
Back

—

Falcon 9 Block 5 | Transporter 11 (Dedicated SSO Rideshare)

Falcon 9 Block 5

Carrier rocket

Space Launch Complex 4E

Spaceport

0

Observations all time

Mission information
Spacecraft name
FLOCK 4BE-19
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 11 (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
409.16 km
Apogee
414.77 km
Inclination
97.4°
Period
92.9 min
Semi-major axis
6789.9 km
Velocity
7.66 km/s
Orbital elements
TLE source
Celestrak
TLE updated
2026-10-12 05:08:35 UTC
Two-line elements (TLE)
1 60563U 24149CZ  26284.93845005  .00033914  00000-0  59135-3 0  9992
2 60563  97.3685  12.5053 0004280 213.0453 147.0532 15.50646055120471
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 16:42:46 FLOCK 4BE-19
NORAD 60563 		OBJECT C
NORAD 60747 		4.676 7.78 1.8e-07
2026-10-16 15:57:59 FLOCK 4BE-19
NORAD 60563 		3CAT-5A
NORAD 46292 		1.152 3.25 3.3e-06
2026-10-17 04:23:48 FLOCK 4BE-19
NORAD 60563 		OBJECT L
NORAD 64886 		3.894 12.71 1.8e-07
2026-10-17 04:59:46 FLOCK 4BE-19
NORAD 60563 		COSMOS 394
NORAD 4922 		4.940 14.38 8.4e-08
2026-10-17 21:22:22 OBJECT F
NORAD 57585 		FLOCK 4BE-19
NORAD 60563 		4.222 0.19 2.5e-07
2026-10-17 22:30:15 GHGSAT-C7
NORAD 56209 		FLOCK 4BE-19
NORAD 60563 		3.459 15.19 1.3e-07
2026-10-18 00:03:07 GHGSAT-C7
NORAD 56209 		FLOCK 4BE-19
NORAD 60563 		3.618 15.19 1.2e-07
2026-10-18 00:49:32 GHGSAT-C7
NORAD 56209 		FLOCK 4BE-19
NORAD 60563 		4.670 15.21 7.2e-08

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