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TRANSPORTER-17 OBJECT BE

In orbit NORAD 69921 BOTC-5446-2914-7208-9475

Observations 0
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Falcon 9 Block 5 | Transporter 17 (Dedicated SSO Rideshare)

Falcon 9 Block 5

Carrier rocket

Space Launch Complex 4E

Spaceport

0

Observations all time

Mission information
Spacecraft name
TRANSPORTER-17 OBJECT BE
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 17 (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
583.42 km
Apogee
591.68 km
Inclination
97.7°
Period
96.5 min
Semi-major axis
6965.7 km
Velocity
7.56 km/s
Orbital elements
TLE source
Celestrak
TLE updated
2026-10-10 20:57:00 UTC
Two-line elements (TLE)
1 69921U 26156BE  26283.23237910  .00002945  00000-0  29321-3 0  9995
2 69921  97.7450 182.1497 0005974 190.5944 169.5151 14.92378889 14158
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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 19:45:10 TRANSPORTER-17 OBJECT BE
NORAD 69921 		CZ-2D DEB
NORAD 44612 		4.505 11.57 1.5e-07
2026-10-12 03:16:29 TRANSPORTER-17 OBJECT BE
NORAD 69921 		FENGYUN 1C DEB
NORAD 33678 		4.482 14.96 8.2e-08
2026-10-12 07:36:01 TRANSPORTER-17 OBJECT BE
NORAD 69921 		PSLV DEB
NORAD 27124 		4.323 14.92 8.6e-08
2026-10-12 14:13:39 YAOGAN-3
NORAD 32289 		TRANSPORTER-17 OBJECT BE
NORAD 69921 		1.877 13.57 6.7e-07
2026-10-12 23:03:22 XINZHENGCHENG 01
NORAD 68414 		TRANSPORTER-17 OBJECT BE
NORAD 69921 		2.232 4.47 8.5e-07
2026-10-13 14:32:29 HUBBLE 7
NORAD 64592 		TRANSPORTER-17 OBJECT BE
NORAD 69921 		3.404 14.32 1.7e-07
2026-10-13 22:14:56 ARCTIC WEATHER SATELLITE
NORAD 60543 		TRANSPORTER-17 OBJECT BE
NORAD 69921 		4.597 14.91 7.7e-08
2026-10-15 07:06:57 TRANSPORTER-17 OBJECT BE
NORAD 69921 		DELTA 2 R/B(1)
NORAD 21891 		4.512 12.74 6.4e-07
2026-10-15 18:37:40 TRANSPORTER-17 OBJECT BE
NORAD 69921 		THOR ABLESTAR DEB
NORAD 351 		3.293 10.72 3.0e-07
2026-10-16 01:45:52 TRANSPORTER-17 OBJECT BE
NORAD 69921 		COSMOS 434 DEB
NORAD 5426 		3.465 8.90 3.1e-07
2026-10-16 03:41:18 SATORO-T3
NORAD 64589 		TRANSPORTER-17 OBJECT BE
NORAD 69921 		4.901 14.32 8.3e-08
2026-10-16 06:04:12 TRANSPORTER-17 OBJECT BE
NORAD 69921 		COSMOS 2251 DEB
NORAD 34854 		0.769 10.57 5.6e-06
2026-10-16 11:37:35 R5-S9
NORAD 69901 		TRANSPORTER-17 OBJECT BE
NORAD 69921 		2.975 0.02 5.0e-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