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FLOCK 4Q-27

In orbit NORAD 58282 AVWW-8644-0459-9021-9122

Satellite appearance

Falcon 9 Block 5

Carrier rocket

Space Launch Complex 4E

Spaceport

0

Observations all time

Mission information
Spacecraft name
FLOCK 4Q-27
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
380.05 km
Apogee
386.41 km
Inclination
97.4°
Period
92.3 min
Semi-major axis
6761.4 km
Velocity
7.69 km/s
Orbital elements
TLE source
Celestrak
TLE updated
2026-08-28 08:35:48 UTC
Two-line elements (TLE)
1 58282U 23174AC  26239.69333220  .00028979  00000-0  35301-3 0  9992
2 58282 97.3763 332.8368 0004702 238.7449 121.3348 15.60463663156885
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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 05:35:55 STARLINK-11514
NORAD 62514
FLOCK 4Q-27
NORAD 58282
4.589 14.48 2.9e-06
2026-10-13 06:21:42 STARLINK-11514
NORAD 62514
FLOCK 4Q-27
NORAD 58282
4.602 14.49 2.9e-06
2026-10-13 11:41:44 STARLINK-11516
NORAD 62522
FLOCK 4Q-27
NORAD 58282
2.398 14.48 1.1e-05
2026-10-13 12:27:31 STARLINK-11516
NORAD 62522
FLOCK 4Q-27
NORAD 58282
1.279 14.48 3.8e-05
2026-10-13 18:43:17 STARLINK-11689
NORAD 64241
FLOCK 4Q-27
NORAD 58282
2.074 8.70 2.6e-05
2026-10-13 19:13:02 STARLINK-11389
NORAD 62091
FLOCK 4Q-27
NORAD 58282
3.189 14.02 6.7e-06
2026-10-13 21:31:45 STARLINK-11404
NORAD 62019
FLOCK 4Q-27
NORAD 58282
4.360 6.43 6.5e-06
2026-10-15 01:51:17 STARLINK-11731
NORAD 64371
FLOCK 4Q-27
NORAD 58282
4.620 14.49 2.9e-06
2026-10-15 02:37:02 STARLINK-11731
NORAD 64371
FLOCK 4Q-27
NORAD 58282
4.444 14.49 3.1e-06
2026-10-15 07:29:24 SITRO-AIS 45
NORAD 61788
FLOCK 4Q-27
NORAD 58282
3.367 14.53 1.8e-07
2026-10-15 10:07:40 STARLINK-11484
NORAD 62277
FLOCK 4Q-27
NORAD 58282
2.952 14.06 7.8e-06
2026-10-15 10:19:34 STARLINK-11407
NORAD 61939
FLOCK 4Q-27
NORAD 58282
4.375 6.11 6.5e-06
2026-10-16 00:38:44 STARLINK-11508
NORAD 62515
FLOCK 4Q-27
NORAD 58282
4.130 14.29 3.8e-06
2026-10-16 01:24:29 STARLINK-11508
NORAD 62515
FLOCK 4Q-27
NORAD 58282
1.341 14.27 3.6e-05
2026-10-16 03:08:27 STARLINK-11598
NORAD 63113
FLOCK 4Q-27
NORAD 58282
4.013 8.08 7.2e-06
2026-10-16 15:18:46 STARLINK-11522
NORAD 63141
FLOCK 4Q-27
NORAD 58282
1.377 7.62 6.2e-05
2026-10-16 19:07:35 STARLINK-11522
NORAD 63141
FLOCK 4Q-27
NORAD 58282
3.795 7.66 8.2e-06
2026-10-17 05:02:46 STARLINK-11185
NORAD 62588
FLOCK 4Q-27
NORAD 58282
3.318 14.24 5.9e-06
2026-10-17 19:34:57 STARLINK-11667
NORAD 63550
FLOCK 4Q-27
NORAD 58282
4.958 13.51 3.0e-06
2026-10-17 20:20:41 STARLINK-11667
NORAD 63550
FLOCK 4Q-27
NORAD 58282
4.643 13.54 3.5e-06
2026-10-18 00:34:35 STARLINK-11563
NORAD 63053
FLOCK 4Q-27
NORAD 58282
4.655 11.27 4.5e-06
2026-10-18 02:51:42 STARLINK-11563
NORAD 63053
FLOCK 4Q-27
NORAD 58282
3.104 11.24 1.0e-05

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