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AC1-003

In orbit NORAD 66689 ARUO-2168-8360-8839-5781

Falcon 9 Block 5

Carrier rocket

Space Launch Complex 4E

Spaceport

0

Observations all time

Mission information
Spacecraft name
AC1-003
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
2025-11-28 18:44:30
Separation time
2025-11-28 20:03:47
Satellite appearance
Data for the last 30 days
Orbital parameters of the satellite
Perigee
505.49 km
Apogee
508.30 km
Inclination
97.4°
Period
94.8 min
Semi-major axis
6885.0 km
Velocity
7.61 km/s
Orbital elements
TLE source
Celestrak
TLE updated
2026-10-14 14:09:04 UTC
Two-line elements (TLE)
1 66689U 25276Z   26287.13536214  .00002332  00000-0  11586-3 0  9991
2 66689 97.4091 358.1286 0002040 355.0614 5.0600 15.18647718 48450
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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
2026-10-15 17:07:36 AC1-003
NORAD 66689
HYDRA-3
NORAD 69022
4.590 15.08 7.5e-08
2026-10-16 04:32:45 AC1-003
NORAD 66689
NOAA 16 DEB
NORAD 41267
4.532 14.53 9.4e-08
2026-10-16 16:26:43 AC1-003
NORAD 66689
ELECTRON KICK STAGE R/B
NORAD 45728
3.266 13.97 2.1e-07
2026-10-16 23:04:06 AC1-003
NORAD 66689
ELECTRON KICK STAGE R/B
NORAD 58579
2.505 10.43 5.4e-07
2026-10-18 12:47:03 AC1-003
NORAD 66689
PEGASUS DEB
NORAD 39922
4.259 15.00 9.0e-08
2026-10-18 13:32:11 KONDOR-FKA NO. 1
NORAD 56756
AC1-003
NORAD 66689
4.525 13.19 1.2e-07
2026-10-18 14:19:37 KONDOR-FKA NO. 1
NORAD 56756
AC1-003
NORAD 66689
2.061 13.16 6.0e-07
2026-10-19 00:32:58 AC1-003
NORAD 66689
SL-16 DEB
NORAD 39708
4.441 7.82 2.0e-07
2026-10-20 14:20:04 AC1-003
NORAD 66689
AVUM R/B
NORAD 49467
2.124 15.15 3.3e-07
2026-10-21 00:52:51 IOD-2
NORAD 64538
AC1-003
NORAD 66689
4.362 5.49 2.2e-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