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FLOCK 4BE-25

In orbit NORAD 60487 OHMJ-8086-3703-4570-2710

Observations 0
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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-25
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
433.77 km
Apogee
437.51 km
Inclination
97.4°
Period
93.4 min
Semi-major axis
6813.8 km
Velocity
7.65 km/s
Orbital elements
TLE source
Celestrak
TLE updated
2026-10-10 12:56:49 UTC
Two-line elements (TLE)
1 60487U 24149V   26283.19904220  .00019696  00000-0  45570-3 0  9998
2 60487  97.3741   7.3410 0002747 174.0946 186.0334 15.42508692119945
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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
2026-10-11 07:38:07 FLOCK 4BE-25
NORAD 60487 		TRANSPORTER-11 OBJECT AU
NORAD 60510 		1.003 0.09 4.4e-06
2026-10-12 10:55:10 FLOCK 4BE-25
NORAD 60487 		FENGYUN 1C DEB
NORAD 30082 		3.837 11.31 2.1e-07
2026-10-14 11:57:29 FLOCK 4BE-25
NORAD 60487 		FENGYUN 1C DEB
NORAD 33687 		3.899 1.39 2.9e-07
2026-10-15 15:10:05 CUBEL
NORAD 47448 		FLOCK 4BE-25
NORAD 60487 		3.574 4.49 3.3e-07
2026-10-16 04:23:52 FLOCK 4BE-25
NORAD 60487 		OBJECT J
NORAD 68206 		3.805 3.23 3.0e-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