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TRANSPORTER-16 OBJECT AA

In orbit NORAD 68440 EDMG-2023-1089-8239-7078

Observations 0
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Falcon 9 Block 5 | Transporter 16 (Dedicated SSO Rideshare)

Falcon 9 Block 5

Carrier rocket

Space Launch Complex 4E

Spaceport

0

Observations all time

Mission information
Spacecraft name
TRANSPORTER-16 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
Launch
Falcon 9 Block 5 | Transporter 16 (Dedicated SSO Rideshare)
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
486.28 km
Apogee
491.38 km
Inclination
97.5°
Period
94.4 min
Semi-major axis
6867.0 km
Velocity
7.61 km/s
Orbital elements
TLE source
Celestrak
TLE updated
2026-10-14 06:09:05 UTC
Two-line elements (TLE)
1 68440U 26067AA  26286.86033619  .00024473  00000-0  99175-3 0  9997
2 68440  97.4642 244.4556 0003718  54.1485 306.0097 15.24640138 30004
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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
2026-10-16 05:39:21 JILIN-1 10
NORAD 43946 		TRANSPORTER-16 OBJECT AA
NORAD 68440 		4.784 14.26 9.1e-08
2026-10-16 05:41:38 ALSAT-3B
NORAD 67646 		TRANSPORTER-16 OBJECT AA
NORAD 68440 		4.397 12.78 1.4e-07
2026-10-17 00:09:34 VIGORIDE-3
NORAD 52760 		TRANSPORTER-16 OBJECT AA
NORAD 68440 		4.889 15.08 6.6e-08
2026-10-17 00:39:57 SPACEEYE-T1
NORAD 63229 		TRANSPORTER-16 OBJECT AA
NORAD 68440 		1.484 8.35 1.7e-06
2026-10-17 20:27:40 STARLINK-5592
NORAD 55741 		TRANSPORTER-16 OBJECT AA
NORAD 68440 		2.729 14.76 7.2e-06
2026-10-18 13:36:23 ZIYUAN 3-02 (ZY 3-02)
NORAD 41556 		TRANSPORTER-16 OBJECT AA
NORAD 68440 		3.813 12.77 1.9e-07
2026-10-18 15:57:48 FLOCK 4G-33
NORAD 62685 		TRANSPORTER-16 OBJECT AA
NORAD 68440 		2.466 13.15 4.2e-07
2026-10-20 10:47:41 STARLINK-5147
NORAD 53985 		TRANSPORTER-16 OBJECT AA
NORAD 68440 		4.130 6.87 7.1e-06
2026-10-20 12:22:15 STARLINK-5147
NORAD 53985 		TRANSPORTER-16 OBJECT AA
NORAD 68440 		4.205 6.85 6.8e-06
2026-10-20 18:04:44 TRANSPORTER-16 OBJECT AA
NORAD 68440 		DELTA 1 DEB
NORAD 10234 		4.074 13.52 1.5e-07
2026-10-20 22:19:35 GAOFEN-11 03
NORAD 49492 		TRANSPORTER-16 OBJECT AA
NORAD 68440 		3.211 9.85 3.4e-07
2026-10-20 23:06:50 GAOFEN-11 03
NORAD 49492 		TRANSPORTER-16 OBJECT AA
NORAD 68440 		4.041 9.88 2.1e-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