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FLOCK 4BE-18

In orbit NORAD 60480 AGFW-2657-9692-7615-8668

Falcon 9 Block 5

Carrier rocket

Space Launch Complex 4E

Spaceport

0

Observations all time

Mission information
Spacecraft name
FLOCK 4BE-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
421.45 km
Apogee
426.77 km
Inclination
97.4°
Period
93.1 min
Semi-major axis
6802.2 km
Velocity
7.64 km/s
Orbital elements
TLE source
Celestrak
TLE updated
2026-10-11 04:56:38 UTC
Two-line elements (TLE)
1 60480U 24149N   26283.90950663  .00041982  00000-0  84635-3 0  9990
2 60480 97.3670 9.1303 0003909 174.2719 185.8576 15.46428503120168
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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
2026-10-12 08:45:54 FLOCK 4BE-18
NORAD 60480
CZ-2D R/B
NORAD 59396
4.683 7.96 1.8e-07
2026-10-12 09:32:36 FLOCK 4BE-18
NORAD 60480
CZ-2D R/B
NORAD 59396
3.908 7.95 2.5e-07
2026-10-12 14:46:24 ISS (NAUKA)
NORAD 49044
FLOCK 4BE-18
NORAD 60480
3.748 9.62 2.5e-07
2026-10-12 14:46:24 ISS (ZARYA)
NORAD 25544
FLOCK 4BE-18
NORAD 60480
3.748 9.62 1.5e-05
2026-10-12 14:46:24 ISS (UNITY)
NORAD 25575
FLOCK 4BE-18
NORAD 60480
3.748 9.62 3.3e-06
2026-10-12 14:46:24 ISS (ZVEZDA)
NORAD 26400
FLOCK 4BE-18
NORAD 60480
3.748 9.62 1.9e-05
2026-10-12 14:46:24 ISS (DESTINY)
NORAD 26700
FLOCK 4BE-18
NORAD 60480
3.748 9.62 2.5e-06
2026-10-12 14:46:24 POISK
NORAD 36086
FLOCK 4BE-18
NORAD 60480
3.748 9.62 2.5e-07
2026-10-12 14:46:24 FLOCK 4BE-18
NORAD 60480
CREW DRAGON 13
NORAD 100882
3.624 9.62 2.7e-07
2026-10-12 14:46:24 FLOCK 4BE-18
NORAD 60480
CYGNUS NG-24
NORAD 68689
3.624 9.62 2.7e-07
2026-10-12 14:46:24 FLOCK 4BE-18
NORAD 60480
PROGRESS-MS 34
NORAD 68837
3.624 9.62 2.7e-07
2026-10-12 14:46:24 FLOCK 4BE-18
NORAD 60480
SOYUZ-MS 29
NORAD 100057
3.624 9.62 2.7e-07
2026-10-12 14:46:24 FLOCK 4BE-18
NORAD 60480
PROGRESS-MS 35
NORAD 100712
3.624 9.62 2.7e-07
2026-10-12 20:48:34 FLOCK 4BE-18
NORAD 60480
TRANSPORTER-6 OBJECT H
NORAD 55016
3.771 2.73 3.1e-07
2026-10-13 07:40:17 NUSAT-26 (M SOMERVILLE)
NORAD 52184
FLOCK 4BE-18
NORAD 60480
0.664 0.90 1.0e-05
2026-10-13 08:26:51 NUSAT-26 (M SOMERVILLE)
NORAD 52184
FLOCK 4BE-18
NORAD 60480
1.841 0.90 1.3e-06
2026-10-13 16:13:49 FLOCK 4BE-18
NORAD 60480
CZ-6A DEB
NORAD 58202
2.965 5.62 4.7e-07
2026-10-14 05:38:28 STARLINK-1215
NORAD 45225
FLOCK 4BE-18
NORAD 60480
3.479 7.42 9.8e-06
2026-10-14 06:44:04 STARLINK-1281
NORAD 45370
FLOCK 4BE-18
NORAD 60480
4.952 14.46 2.5e-06
2026-10-14 16:58:59 FLOCK 4BE-18
NORAD 60480
CZ-6A DEB
NORAD 60630
3.806 15.11 1.1e-07
2026-10-14 21:57:12 FLOCK 4BE-18
NORAD 60480
SHIYAN-32 02
NORAD 66378
4.030 14.44 1.2e-07
2026-10-15 13:51:07 FLOCK 4BE-18
NORAD 60480
BREEZE-M DEB
NORAD 38922
3.989 11.53 2.0e-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