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TRANSPORTER-16 OBJECT Y

In orbit NORAD 68438 DOSD-4831-2865-9677-9294

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 Y
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
490.64 km
Apogee
495.20 km
Inclination
97.5°
Period
94.5 min
Semi-major axis
6871.1 km
Velocity
7.62 km/s
Orbital elements
TLE source
Celestrak
TLE updated
2026-10-14 06:09:05 UTC
Two-line elements (TLE)
1 68438U 26067Y   26286.88233600  .00020077  00000-0  84810-3 0  9994
2 68438  97.4670 244.3281 0003317  38.8417 321.3057 15.23280510 29990
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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 09:42:05 TRANSPORTER-16 OBJECT Y
NORAD 68438 		CZ-4B DEB
NORAD 35573 		4.722 14.68 8.2e-08
2026-10-15 11:21:20 IHI-SAT2
NORAD 66772 		TRANSPORTER-16 OBJECT Y
NORAD 68438 		2.422 12.74 4.6e-07
2026-10-15 21:30:24 STARLINK-5917
NORAD 55942 		TRANSPORTER-16 OBJECT Y
NORAD 68438 		3.188 14.87 5.1e-06
2026-10-15 23:10:54 SCS-01 F
NORAD 63987 		TRANSPORTER-16 OBJECT Y
NORAD 68438 		3.535 12.54 2.2e-07
2026-10-16 19:40:31 SCS-01 L
NORAD 63992 		TRANSPORTER-16 OBJECT Y
NORAD 68438 		1.706 12.55 9.5e-07
2026-10-17 03:33:21 FLOCK 4H-9
NORAD 66712 		TRANSPORTER-16 OBJECT Y
NORAD 68438 		4.704 12.67 1.2e-07
2026-10-17 14:35:25 FLOCK 4H-36
NORAD 66739 		TRANSPORTER-16 OBJECT Y
NORAD 68438 		4.971 12.68 1.1e-07
2026-10-17 19:19:18 SCS-01 K
NORAD 63991 		TRANSPORTER-16 OBJECT Y
NORAD 68438 		0.982 12.54 2.9e-06
2026-10-17 22:30:02 TRANSPORTER-16 OBJECT Y
NORAD 68438 		RASSVET-3 24
NORAD 100090 		4.945 12.92 1.1e-07
2026-10-18 04:47:40 ITASAT
NORAD 43786 		TRANSPORTER-16 OBJECT Y
NORAD 68438 		2.260 10.81 6.4e-07
2026-10-18 07:08:31 FLOCK 4H-20
NORAD 66723 		TRANSPORTER-16 OBJECT Y
NORAD 68438 		4.902 12.72 1.1e-07
2026-10-20 06:38:28 STARLINK-3399
NORAD 51121 		TRANSPORTER-16 OBJECT Y
NORAD 68438 		2.353 12.41 1.5e-05
2026-10-20 15:00:30 CONNECTA IOT-11
NORAD 64557 		TRANSPORTER-16 OBJECT Y
NORAD 68438 		4.278 14.77 9.7e-08
2026-10-20 15:41:19 OBJECT E
NORAD 67750 		TRANSPORTER-16 OBJECT Y
NORAD 68438 		3.519 15.06 1.3e-07
2026-10-21 01:03:17 STARLINK-5857
NORAD 55946 		TRANSPORTER-16 OBJECT Y
NORAD 68438 		1.602 15.14 1.8e-05

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