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AAC-HSI-SAT3

In orbit NORAD 58848 FPOI-0478-7880-8073-3908

Falcon 9 Block 5

Carrier rocket

Space Launch Complex 4E

Spaceport

0

Observations all time

Mission information
Spacecraft name
AAC-HSI-SAT3
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
507.63 km
Apogee
520.86 km
Inclination
97.3°
Period
95.0 min
Semi-major axis
6892.4 km
Velocity
7.61 km/s
Orbital elements
TLE source
Celestrak
TLE updated
2026-10-10 20:56:57 UTC
Two-line elements (TLE)
1 58848U 23174DH  26283.58265883  .00001945  00000-0  10391-3 0  9992
2 58848 97.3277 339.1101 0009570 334.7745 25.3020 15.16221035161389
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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 01:22:20 STARLINK-5598
NORAD 55421
AAC-HSI-SAT3
NORAD 58848
4.487 10.01 5.2e-06
2026-10-11 02:57:22 STARLINK-5598
NORAD 55421
AAC-HSI-SAT3
NORAD 58848
3.007 10.03 1.2e-05
2026-10-11 03:50:13 AAC-HSI-SAT3
NORAD 58848
RADIX-A
NORAD 100941
3.885 1.82 2.9e-07
2026-10-11 05:25:14 AAC-HSI-SAT3
NORAD 58848
TRANSPORTER-18 OBJECT AR
NORAD 100922
1.791 1.82 1.4e-06
2026-10-11 05:45:52 AAC-HSI-SAT3
NORAD 58848
CURIUM ONE
NORAD 60242
4.334 14.96 8.8e-08
2026-10-11 14:54:52 OBJECT AK
NORAD 57037
AAC-HSI-SAT3
NORAD 58848
1.514 6.22 1.8e-06
2026-10-11 16:30:29 AAC-HSI-SAT3
NORAD 58848
TRANSPORTER-18 OBJECT AF
NORAD 100912
3.146 1.82 4.4e-07
2026-10-11 19:40:32 AAC-HSI-SAT3
NORAD 58848
TRANSPORTER-18 OBJECT AK
NORAD 100916
1.627 1.82 1.7e-06
2026-10-11 21:20:55 STARLINK-5920
NORAD 55935
AAC-HSI-SAT3
NORAD 58848
2.343 13.07 1.4e-05
2026-10-12 02:00:40 AAC-HSI-SAT3
NORAD 58848
TRANSPORTER-18 OBJECT AD
NORAD 100910
2.061 1.82 1.0e-06
2026-10-12 08:20:48 AAC-HSI-SAT3
NORAD 58848
TRANSPORTER-18 OBJECT AU
NORAD 100925
2.843 1.82 5.4e-07
2026-10-12 13:05:54 AAC-HSI-SAT3
NORAD 58848
TRANSPORTER-18 OBJECT BA
NORAD 100931
4.473 1.82 2.2e-07
2026-10-12 14:40:56 AAC-HSI-SAT3
NORAD 58848
TRANSPORTER-18 OBJECT BD
NORAD 100934
4.727 1.82 2.0e-07
2026-10-13 08:06:18 AAC-HSI-SAT3
NORAD 58848
TRANSPORTER-18 OBJECT AG
NORAD 100913
3.252 1.82 4.1e-07
2026-10-14 06:16:46 AAC-HSI-SAT3
NORAD 58848
TRANSPORTER-18 OBJECT AN
NORAD 100919
3.007 1.82 4.9e-07
2026-10-14 20:41:15 AAC-HSI-SAT3
NORAD 58848
UNKNOWN
NORAD 87764
4.691 7.72 1.8e-07
2026-10-14 22:07:06 AAC-HSI-SAT3
NORAD 58848
TRANSPORTER-18 OBJECT AL
NORAD 100917
3.320 1.82 4.0e-07
2026-10-15 04:29:52 AAC-HSI-SAT3
NORAD 58848
IRIDE-MS1-EAGLET 2-16
NORAD 68452
4.661 11.41 1.4e-07
2026-10-15 08:21:22 AAC-HSI-SAT3
NORAD 58848
YUNYAO-1 43
NORAD 63344
4.542 13.40 1.2e-07
2026-10-16 01:49:46 AAC-HSI-SAT3
NORAD 58848
OBJECT A
NORAD 60012
4.414 4.56 2.2e-07
2026-10-16 02:48:47 AAC-HSI-SAT3
NORAD 58848
SPACEMOBILE-005
NORAD 61046
4.154 13.49 1.4e-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