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OBJECT BE

In orbit NORAD 100935 QQUP-3406-7306-1408-9273

Observations 0
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Falcon 9 Block 5 | Transporter 18 (Dedicated SSO Rideshare)

Falcon 9 Block 5

Carrier rocket

Space Launch Complex 4E

Spaceport

0

Observations all time

Mission information
Spacecraft name
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 18 (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
503.65 km
Apogee
512.84 km
Inclination
97.4°
Period
94.8 min
Semi-major axis
6886.4 km
Velocity
7.6 km/s
Orbital elements
TLE source
Celestrak
TLE updated
2026-10-14 14:09:06 UTC
Two-line elements (TLE)
1 A0935U 26227BE  26287.13943676  .00004049  00000-0  20120-3 0  9995
2 A0935  97.4428 356.4566 0006686 111.3886 248.8062 15.18205645  1886
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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 01:55:17 SCS-01 E
NORAD 63986 		TRANSPORTER-18 OBJECT BE
NORAD 100935 		3.156 0.09 4.4e-07
2026-10-15 19:12:17 STARLINK-5598
NORAD 55421 		TRANSPORTER-18 OBJECT BE
NORAD 100935 		4.064 12.56 5.1e-06
2026-10-16 00:49:43 SIRION PATHFINDER-2
NORAD 43759 		TRANSPORTER-18 OBJECT BE
NORAD 100935 		2.125 3.02 9.6e-07
2026-10-16 15:05:38 LEMUR-2-THERMORAPTOR
NORAD 63354 		TRANSPORTER-18 OBJECT BE
NORAD 100935 		3.763 10.98 2.3e-07
2026-10-17 06:06:32 TOMORROW-S10
NORAD 67398 		TRANSPORTER-18 OBJECT BE
NORAD 100935 		2.606 8.81 5.4e-07
2026-10-17 23:29:19 TRANSPORTER-18 OBJECT BE
NORAD 100935 		FLOCK 4H-28
NORAD 66731 		4.809 0.28 1.9e-07
2026-10-18 05:35:17 STARLINK-30223
NORAD 57603 		TRANSPORTER-18 OBJECT BE
NORAD 100935 		3.100 9.65 1.1e-05
2026-10-18 05:48:16 OBJECT A
NORAD 65938 		TRANSPORTER-18 OBJECT BE
NORAD 100935 		4.624 1.61 2.1e-07
2026-10-18 06:37:35 DTUSAT-2
NORAD 40030 		TRANSPORTER-18 OBJECT BE
NORAD 100935 		4.637 7.92 1.8e-07
2026-10-18 14:00:10 TRANSPORTER-18 OBJECT BE
NORAD 100935 		TRANSPORTER-18 OBJECT BQ
NORAD 100945 		0.672 0.00 5.7e-06
2026-10-19 02:16:59 STARLINK-5038
NORAD 56472 		TRANSPORTER-18 OBJECT BE
NORAD 100935 		3.003 10.28 1.1e-05
2026-10-20 04:29:44 CFOSAT
NORAD 43662 		TRANSPORTER-18 OBJECT BE
NORAD 100935 		4.238 8.45 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