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TRANSPORTER-16 OBJECT Z

In orbit NORAD 68439 POAT-0740-3502-3084-7533

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 Z
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
492.80 km
Apogee
497.84 km
Inclination
97.5°
Period
94.6 min
Semi-major axis
6873.5 km
Velocity
7.6 km/s
Orbital elements
TLE source
Celestrak
TLE updated
2026-10-14 06:09:05 UTC
Two-line elements (TLE)
1 68439U 26067Z   26286.86536150  .00015923  00000-0  68957-3 0  9997
2 68439  97.4649 244.1639 0003670  49.3197 310.8358 15.22483233 29988
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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 15:16:01 ROADS 1
NORAD 64535 		TRANSPORTER-16 OBJECT Z
NORAD 68439 		4.677 14.81 8.1e-08
2026-10-16 16:03:20 ROADS 1
NORAD 64535 		TRANSPORTER-16 OBJECT Z
NORAD 68439 		4.117 14.77 1.0e-07
2026-10-16 17:37:56 ROADS 1
NORAD 64535 		TRANSPORTER-16 OBJECT Z
NORAD 68439 		4.368 14.77 9.3e-08
2026-10-17 06:26:14 TRANSPORTER-16 OBJECT Z
NORAD 68439 		NOAA 16 DEB
NORAD 41267 		4.063 11.27 1.9e-07
2026-10-17 19:49:15 TRANSPORTER-16 OBJECT Z
NORAD 68439 		KIRARI (OICETS)
NORAD 28809 		0.383 6.74 2.7e-05
2026-10-17 20:31:10 TRANSPORTER-16 OBJECT Z
NORAD 68439 		CZ-6A DEB
NORAD 54307 		4.079 13.51 1.4e-07
2026-10-18 00:23:33 CONNECTA IOT-9
NORAD 64534 		TRANSPORTER-16 OBJECT Z
NORAD 68439 		2.940 14.79 2.1e-07
2026-10-18 01:13:11 TRANSPORTER-16 OBJECT Z
NORAD 68439 		DFH 1
NORAD 4382 		4.455 10.11 1.5e-07
2026-10-18 06:35:31 OBJECT B
NORAD 67747 		TRANSPORTER-16 OBJECT Z
NORAD 68439 		2.852 15.06 2.0e-07
2026-10-18 19:12:49 PROPCUBE 3
NORAD 40973 		TRANSPORTER-16 OBJECT Z
NORAD 68439 		4.872 5.18 1.8e-07
2026-10-19 11:15:40 STARLINK-4622
NORAD 53648 		TRANSPORTER-16 OBJECT Z
NORAD 68439 		4.767 10.18 4.6e-06
2026-10-19 13:32:55 NUSAT-47
NORAD 66743 		TRANSPORTER-16 OBJECT Z
NORAD 68439 		1.854 12.66 7.9e-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