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OBJECT AA

In orbit NORAD 100907 EFUR-6914-3506-9307-8837

Falcon 9 Block 5

Carrier rocket

Space Launch Complex 4E

Spaceport

0

Observations all time

Mission information
Spacecraft name
OBJECT AA
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
510.08 km
Apogee
513.64 km
Inclination
97.4°
Period
94.9 min
Semi-major axis
6890.0 km
Velocity
7.59 km/s
Orbital elements
TLE source
Celestrak
TLE updated
2026-10-14 14:09:06 UTC
Two-line elements (TLE)
1 A0907U 26227AA  26287.14902879  .00004872  00000-0  24978-3 0  9994
2 A0907 97.4396 356.4392 0002562 69.8502 290.3007 15.17014769 1882
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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 04:21:31 TRANSPORTER-18 OBJECT AA
NORAD 100907
FENGYUN 1C DEB
NORAD 30520
3.193 14.70 1.8e-07
2026-10-16 03:29:13 FLAMINGO-1
NORAD 67391
TRANSPORTER-18 OBJECT AA
NORAD 100907
3.620 8.88 2.8e-07
2026-10-16 23:23:42 TRANSPORTER-18 OBJECT AA
NORAD 100907
RE
NORAD 38765
3.925 14.37 1.3e-07
2026-10-17 03:39:18 TRANSPORTER-18 OBJECT AA
NORAD 100907
THORAD AGENA D DEB
NORAD 4157
3.809 15.11 1.1e-07
2026-10-17 06:49:41 TRANSPORTER-18 OBJECT AA
NORAD 100907
TRANSPORTER-18 OBJECT AY
NORAD 100929
1.606 0.00 1.3e-06
2026-10-17 09:54:39 LEGION 5
NORAD 62900
TRANSPORTER-18 OBJECT AA
NORAD 100907
2.124 6.76 8.9e-07
2026-10-17 10:23:12 TRANSPORTER-18 OBJECT AA
NORAD 100907
TRANSPORTER-18 OBJECT AX
NORAD 100928
1.292 0.00 1.7e-06
2026-10-17 10:42:16 LEGION 5
NORAD 62900
TRANSPORTER-18 OBJECT AA
NORAD 100907
1.907 6.75 1.1e-06
2026-10-18 11:50:54 TRANSPORTER-18 OBJECT AA
NORAD 100907
TRANSPORTER-18 OBJECT AE
NORAD 100911
4.831 0.01 1.9e-07
2026-10-18 13:24:44 TRANSPORTER-18 OBJECT AA
NORAD 100907
TRANSPORTER-18 OBJECT AE
NORAD 100911
2.879 0.00 5.3e-07
2026-10-18 14:53:52 TRANSPORTER-18 OBJECT AA
NORAD 100907
TRANSPORTER-18 OBJECT AE
NORAD 100911
1.339 0.00 7.4e-06
2026-10-18 16:17:19 TRANSPORTER-18 OBJECT AA
NORAD 100907
TRANSPORTER-18 OBJECT AE
NORAD 100911
1.141 0.00 7.4e-06
2026-10-18 17:04:23 TRANSPORTER-18 OBJECT AA
NORAD 100907
TRANSPORTER-18 OBJECT AE
NORAD 100911
0.734 0.00 7.4e-06
2026-10-18 17:37:30 TRANSPORTER-18 OBJECT AA
NORAD 100907
TRANSPORTER-18 OBJECT AE
NORAD 100911
1.728 0.00 7.4e-06
2026-10-18 18:48:20 TRANSPORTER-18 OBJECT AA
NORAD 100907
TRANSPORTER-18 OBJECT AE
NORAD 100911
1.474 0.00 7.4e-06
2026-10-18 20:26:08 TRANSPORTER-18 OBJECT AA
NORAD 100907
TRANSPORTER-18 OBJECT AE
NORAD 100911
3.477 0.01 3.6e-07
2026-10-20 02:19:19 TRANSPORTER-18 OBJECT AA
NORAD 100907
COSMOS 397 DEB
NORAD 5094
2.676 14.26 3.0e-07
2026-10-20 12:21:51 DS-EO
NORAD 52935
TRANSPORTER-18 OBJECT AA
NORAD 100907
2.507 10.70 5.3e-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