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FLOCK 4Q-7

In orbit NORAD 58318 LFGM-2421-5458-3698-4343

Observations 0
Satellite appearance

—

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

Falcon 9 Block 5

Carrier rocket

Space Launch Complex 4E

Spaceport

0

Observations all time

Mission information
Spacecraft name
FLOCK 4Q-7
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 9 (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
381.90 km
Apogee
388.63 km
Inclination
97.4°
Period
92.3 min
Semi-major axis
6763.4 km
Velocity
7.68 km/s
Orbital elements
TLE source
Celestrak
TLE updated
2026-08-27 12:35:48 UTC
Two-line elements (TLE)
1 58318U 23174BQ  26239.25177874  .00034080  00000-0  42587-3 0  9999
2 58318  97.3931 333.3847 0004973 229.0391 131.0436 15.59759299156819
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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
2026-10-13 18:52:32 STARLINK-11720
NORAD 64131 		FLOCK 4Q-7
NORAD 58318 		2.353 10.48 1.8e-05
2026-10-14 10:33:57 STARLINK-11134
NORAD 59956 		FLOCK 4Q-7
NORAD 58318 		4.590 13.76 3.4e-06
2026-10-14 14:23:23 STARLINK-11134
NORAD 59956 		FLOCK 4Q-7
NORAD 58318 		4.538 13.78 3.5e-06
2026-10-15 09:12:29 STARLINK-11102
NORAD 60065 		FLOCK 4Q-7
NORAD 58318 		2.805 14.74 7.3e-06
2026-10-15 21:45:41 STARLINK-11088
NORAD 59709 		FLOCK 4Q-7
NORAD 58318 		3.284 9.32 1.0e-05
2026-10-16 04:37:38 STARLINK-11134
NORAD 59956 		FLOCK 4Q-7
NORAD 58318 		3.319 14.16 6.0e-06
2026-10-16 06:55:17 STARLINK-11134
NORAD 59956 		FLOCK 4Q-7
NORAD 58318 		3.722 14.21 4.7e-06
2026-10-16 08:27:02 STARLINK-11134
NORAD 59956 		FLOCK 4Q-7
NORAD 58318 		3.788 14.22 4.6e-06

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