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ACCENTURE-1

In orbit NORAD 66767 FTJT-2036-5505-2802-8572

Falcon 9 Block 5

Carrier rocket

Space Launch Complex 4E

Spaceport

0

Observations all time

Mission information
Spacecraft name
ACCENTURE-1
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
499.40 km
Apogee
502.31 km
Inclination
97.4°
Period
94.7 min
Semi-major axis
6879.0 km
Velocity
7.61 km/s
Orbital elements
TLE source
Celestrak
TLE updated
2026-10-10 20:56:59 UTC
Two-line elements (TLE)
1 66767U 25276DF  26283.51080785  .00003018  00000-0  14063-3 0  9998
2 66767 97.4065 355.1538 0002121 109.6271 250.5194 15.20649605 47956
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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 02:38:19 FGN-100-D2
NORAD 66299
ACCENTURE-1
NORAD 66767
2.238 13.64 4.7e-07
2026-10-12 01:14:36 ACCENTURE-1
NORAD 66767
SPACEMOBILE-006
NORAD 67232
4.712 14.52 8.7e-08
2026-10-12 08:24:39 ACCENTURE-1
NORAD 66767
EYCORE-1
NORAD 69011
2.729 15.08 2.1e-07
2026-10-12 09:59:23 ACCENTURE-1
NORAD 66767
EYCORE-1
NORAD 69011
0.448 15.08 7.8e-06
2026-10-12 11:34:07 ACCENTURE-1
NORAD 66767
EYCORE-1
NORAD 69011
3.583 15.08 1.2e-07
2026-10-14 04:37:44 ACCENTURE-1
NORAD 66767
RAVEN
NORAD 69016
4.958 15.07 6.4e-08
2026-10-14 04:48:32 FGN-100-D2
NORAD 66299
ACCENTURE-1
NORAD 66767
1.828 14.19 6.3e-07
2026-10-14 06:12:27 ACCENTURE-1
NORAD 66767
RAVEN
NORAD 69016
1.784 15.07 4.9e-07
2026-10-14 07:47:11 ACCENTURE-1
NORAD 66767
RAVEN
NORAD 69016
4.661 15.07 7.2e-08
2026-10-14 08:16:24 HJ-2F
NORAD 57519
ACCENTURE-1
NORAD 66767
3.695 8.50 2.8e-07
2026-10-15 00:01:42 ZHANGHENG 1-02 (CSES-2)
NORAD 64393
ACCENTURE-1
NORAD 66767
3.210 6.69 3.9e-07
2026-10-15 02:23:49 ZHANGHENG 1-02 (CSES-2)
NORAD 64393
ACCENTURE-1
NORAD 66767
1.259 6.67 2.5e-06
2026-10-15 04:46:44 CO3D 4
NORAD 64901
ACCENTURE-1
NORAD 66767
2.867 0.71 5.4e-07
2026-10-15 22:09:03 CO3D 3
NORAD 64900
ACCENTURE-1
NORAD 66767
3.597 0.71 3.4e-07
2026-10-15 22:56:26 CO3D 3
NORAD 64900
ACCENTURE-1
NORAD 66767
3.382 0.71 3.9e-07
2026-10-16 18:46:56 ACCENTURE-1
NORAD 66767
COSMOS 2251 DEB
NORAD 34449
3.416 14.88 1.5e-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