RU | EN | ZH --:-- UTC Sign in
Back

BRO-19

In orbit NORAD 68422 ZLVU-1189-2777-4843-4951

Observations 21
Go to map
Back

2026

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

Falcon 9 Block 5

Carrier rocket

Space Launch Complex 4E

Spaceport

21

Observations all time

Mission information
Spacecraft name
BRO-19
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
2026-03-30 11:02:00
Separation time
Satellite appearance
Data for the last 30 days
Orbital parameters of the satellite
Perigee
503.32 km
Apogee
505.61 km
Inclination
97.5°
Period
94.8 min
Semi-major axis
6882.6 km
Velocity
7.59 km/s
Orbital elements
TLE source
Celestrak
TLE updated
2026-10-12 13:08:42 UTC
Two-line elements (TLE)
1 68422U 26067G   26285.29486396  .00003567  00000-0  17148-3 0  9998
2 68422  97.4628 242.2029 0001730 116.8701 243.2711 15.19458849 29720
Copy content
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
2026-10-13 09:05:55 BRO-19
NORAD 68422 		FALCON 9 DEB
NORAD 48610 		1.635 5.91 1.5e-06
2026-10-15 01:48:07 LILIUM-3
NORAD 66770 		BRO-19
NORAD 68422 		1.887 12.72 7.6e-07
2026-10-15 02:35:31 LILIUM-3
NORAD 66770 		BRO-19
NORAD 68422 		3.280 12.69 2.5e-07
2026-10-15 12:08:09 BRO-19
NORAD 68422 		NUSAT-54 (BRANCA MARQUES)
NORAD 68442 		3.907 0.02 2.9e-07
2026-10-15 12:55:34 BRO-19
NORAD 68422 		NUSAT-54 (BRANCA MARQUES)
NORAD 68442 		2.133 0.02 9.7e-07
2026-10-15 12:56:04 BRO-19
NORAD 68422 		HELIOS
NORAD 69021 		4.614 7.70 1.8e-07
2026-10-16 01:34:42 BRO-19
NORAD 68422 		JEN-1
NORAD 69006 		3.562 7.69 3.1e-07
2026-10-16 10:03:50 SPACEMOBILE-004
NORAD 61049 		BRO-19
NORAD 68422 		4.519 13.74 1.1e-07
2026-10-17 08:07:21 OBJECT A
NORAD 67746 		BRO-19
NORAD 68422 		3.899 15.02 1.1e-07
2026-10-17 09:42:09 OBJECT A
NORAD 67746 		BRO-19
NORAD 68422 		4.470 15.02 8.0e-08
2026-10-17 17:34:17 STARLINK-3107
NORAD 49171 		BRO-19
NORAD 68422 		4.554 15.10 2.3e-06
2026-10-17 22:01:45 STARLINK-5002
NORAD 53922 		BRO-19
NORAD 68422 		4.407 14.22 3.3e-06
2026-10-19 04:29:18 SKYBEE-A02
NORAD 64544 		BRO-19
NORAD 68422 		3.700 14.76 1.3e-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