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2024-018A

In orbit NORAD 58849 UZCM-7531-2216-8681-8632 Iran

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2024

Launch

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Observations all time

Mission information
Spacecraft name
2024-018A
Other names
2024-018A
Status
Active
The satellite is in orbit
The network has not received data from this satellite for a long time
Launch and timeline
Launch time
2024-01-28 00:00:00
Separation time
2024-01-28 00:00:00
Satellite appearance
Data for the last 30 days
Orbital parameters of the satellite
Perigee
456.31 km
Apogee
1060.27 km
Inclination
58.7°
Period
100.0 min
Semi-major axis
7136.4 km
Velocity
7.73 km/s
Orbital elements
TLE source
Celestrak
TLE updated
2026-10-11 04:56:38 UTC
Two-line elements (TLE)
1 58849U 24018A   26284.00477174  .00000989  00000-0  13343-3 0  9994
2 58849  58.6889 183.8526 0423153 242.0497 113.7095 14.39885770141856
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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 20:34:12 OBJECT A
NORAD 58849 		THORAD AGENA D DEB
NORAD 42543 		4.338 12.19 1.4e-07
2026-10-11 23:00:27 OBJECT A
NORAD 58849 		LYNK TOWER 5
NORAD 59121 		3.370 13.03 2.3e-07
2026-10-12 02:15:12 OBJECT A
NORAD 58849 		STARLINK-34400
NORAD 64463 		4.217 1.89 7.4e-06
2026-10-12 07:09:32 OBJECT A
NORAD 58849 		STARLINK-35443
NORAD 66339 		2.328 9.86 2.0e-05
2026-10-12 10:52:42 OBJECT A
NORAD 58849 		KUIPER-00119
NORAD 65155 		1.273 9.95 2.1e-06
2026-10-13 09:30:02 IRIDIUM 122
NORAD 42957 		OBJECT A
NORAD 58849 		4.061 14.04 1.2e-07
2026-10-13 15:00:03 OBJECT A
NORAD 58849 		PEGASUS R/B
NORAD 31305 		4.765 11.19 1.4e-07
2026-10-13 19:52:49 STARLINK-31136
NORAD 58772 		OBJECT A
NORAD 58849 		2.951 9.60 1.2e-05
2026-10-13 22:11:20 OBJECT A
NORAD 58849 		SL-8 DEB
NORAD 24818 		4.741 13.78 9.1e-08
2026-10-13 23:29:12 STARLINK-6056
NORAD 56813 		OBJECT A
NORAD 58849 		3.839 2.77 8.9e-06
2026-10-14 00:52:57 STARLINK-5205
NORAD 54202 		OBJECT A
NORAD 58849 		4.151 9.47 6.3e-06
2026-10-15 15:30:26 OBJECT A
NORAD 58849 		NIGERIASAT-1
NORAD 27941 		3.457 7.46 3.3e-07
2026-10-16 01:26:17 OBJECT A
NORAD 58849 		OBJECT C
NORAD 62731 		4.907 9.37 1.5e-07
2026-10-16 04:36:04 OBJECT A
NORAD 58849 		STARLINK-37971
NORAD 100482 		2.417 4.85 2.2e-05
2026-10-16 06:05:58 OBJECT A
NORAD 58849 		TRANSPORTER-18 OBJECT N
NORAD 100895 		2.430 14.91 3.0e-07
2026-10-16 07:47:16 OBJECT A
NORAD 58849 		FLOCK 4H-4
NORAD 66707 		1.444 14.89 8.6e-07
2026-10-16 16:02:44 OBJECT A
NORAD 58849 		HELIOS 2A
NORAD 28492 		4.462 14.93 8.6e-08
2026-10-16 21:19:04 OBJECT A
NORAD 58849 		STARLINK-36833
NORAD 68109 		4.759 10.86 4.4e-06
2026-10-16 21:28:13 SHIJIAN-6 01B (SJ-6 01B)
NORAD 28414 		OBJECT A
NORAD 58849 		4.353 14.26 1.1e-07
2026-10-17 00:29:06 OBJECT A
NORAD 58849 		OBJECT AS
NORAD 67288 		3.566 14.83 1.4e-07
2026-10-17 05:32:55 OBJECT A
NORAD 58849 		STARLINK-35791
NORAD 66896 		3.250 9.02 1.1e-05
2026-10-17 09:01:24 OBJECT A
NORAD 58849 		STARLINK-34568
NORAD 64717 		4.504 6.21 6.1e-06
2026-10-17 13:53:35 OBJECT A
NORAD 58849 		STARLINK-32442
NORAD 61729 		3.561 1.71 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