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AAC-AIS-SAT3

In orbit NORAD 58997 SAID-7205-3683-8017-9859 United Kingdom

Observations 0
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2023

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
AAC-AIS-SAT3
Other names
2023-174DJ
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
2023-11-11 00:00:00
Separation time
2023-11-11 00:00:00
Satellite appearance
Data for the last 30 days
Orbital parameters of the satellite
Perigee
606.19 km
Apogee
613.25 km
Inclination
97.6°
Period
97.0 min
Semi-major axis
6987.8 km
Velocity
7.55 km/s
Orbital elements
TLE source
Celestrak
TLE updated
2026-10-11 12:56:43 UTC
Two-line elements (TLE)
1 58997U 23174DJ  26284.29990333  .00003606  00000-0  42564-3 0  9994
2 58997  97.6124 327.9219 0005043 304.5143  55.5596 14.85286012158381
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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 06:21:49 AAC-AIS-SAT3
NORAD 58997 		FENGYUN 1C DEB
NORAD 38513 		2.462 14.53 3.1e-07
2026-10-12 11:43:39 AAC-AIS-SAT3
NORAD 58997 		SL-8 DEB
NORAD 15756 		3.603 5.00 3.2e-07
2026-10-12 13:27:00 AAC-AIS-SAT3
NORAD 58997 		NOAA 16 DEB
NORAD 42341 		1.436 12.90 1.3e-06
2026-10-12 17:32:34 AAC-AIS-SAT3
NORAD 58997 		IRIDIUM 33 DEB
NORAD 36490 		2.155 11.33 6.7e-07
2026-10-13 01:28:14 AAC-AIS-SAT3
NORAD 58997 		FENGYUN 1C DEB
NORAD 31892 		3.890 14.74 1.2e-07
2026-10-14 08:39:27 AAC-AIS-SAT3
NORAD 58997 		XINZHENGCHENG-01
NORAD 68412 		4.542 15.09 7.2e-08
2026-10-14 16:25:24 AAC-AIS-SAT3
NORAD 58997 		DELTA 1 DEB
NORAD 8319 		3.048 2.35 4.7e-07
2026-10-15 04:09:41 AAC-AIS-SAT3
NORAD 58997 		TITAN 3C TRANSTAGE DEB
NORAD 3373 		3.707 13.66 1.7e-07
2026-10-15 10:09:06 AAC-AIS-SAT3
NORAD 58997 		COSMOS 2251 DEB
NORAD 35661 		3.466 14.40 1.6e-07
2026-10-16 14:06:26 AAC-AIS-SAT3
NORAD 58997 		SL-14 R/B
NORAD 16263 		2.999 15.10 3.9e-07
2026-10-17 01:51:14 TIANHUI 5B
NORAD 58201 		AAC-AIS-SAT3
NORAD 58997 		4.066 4.83 2.5e-07
2026-10-17 09:46:16 AAC-AIS-SAT3
NORAD 58997 		XINZHENGCHENG 01
NORAD 68414 		0.722 15.07 2.8e-06
2026-10-17 11:33:41 AAC-AIS-SAT3
NORAD 58997 		ALOS DEB
NORAD 35418 		4.200 6.49 2.3e-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