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

BRO-19

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

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
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
503.14 km
Apogee
505.67 km
Inclination
97.5°
Period
94.8 min
Semi-major axis
6882.5 km
Velocity
7.61 km/s
Orbital elements
TLE source
Celestrak
TLE updated
2026-10-14 14:09:05 UTC
Two-line elements (TLE)
1 68422U 26067G   26287.13879278  .00003219  00000-0  15498-3 0  9998
2 68422 97.4634 244.0252 0001832 116.4272 243.7151 15.19471923 30001
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
2026-10-15 17:36:23 OBJECT AC
NORAD 67274
BRO-19
NORAD 68422
4.598 12.78 1.3e-07
2026-10-16 01:34:44 BRO-19
NORAD 68422
JEN-1
NORAD 69006
1.476 7.69 1.8e-06
2026-10-16 22:42:09 SPACEMOBILE-004
NORAD 61049
BRO-19
NORAD 68422
3.412 13.86 1.9e-07
2026-10-17 00:16:55 SPACEMOBILE-004
NORAD 61049
BRO-19
NORAD 68422
2.792 13.87 2.9e-07
2026-10-17 05:57:37 SCS-01 F
NORAD 63987
BRO-19
NORAD 68422
3.377 12.60 2.4e-07
2026-10-17 08:07:23 OBJECT A
NORAD 67746
BRO-19
NORAD 68422
4.003 15.02 1.0e-07
2026-10-17 09:42:11 OBJECT A
NORAD 67746
BRO-19
NORAD 68422
4.832 15.02 6.9e-08
2026-10-17 15:30:38 BRO-19
NORAD 68422
CAS500-2
NORAD 69013
3.906 7.72 2.5e-07
2026-10-18 00:59:36 BRO-19
NORAD 68422
BALKAN-2
NORAD 69024
3.561 7.69 3.1e-07
2026-10-18 10:49:44 STARLINK-33998
NORAD 63951
BRO-19
NORAD 68422
4.357 15.12 2.5e-06
2026-10-18 20:44:58 BRO-19
NORAD 68422
JACKAL-004
NORAD 69012
4.857 7.58 1.7e-07
2026-10-19 00:32:20 SKYBEE-A02
NORAD 64544
BRO-19
NORAD 68422
4.537 14.79 8.6e-08
2026-10-19 02:54:32 SKYBEE-A02
NORAD 64544
BRO-19
NORAD 68422
2.884 14.76 2.1e-07
2026-10-19 05:22:29 SCS-01 E
NORAD 63986
BRO-19
NORAD 68422
1.748 12.59 9.0e-07
2026-10-19 10:06:40 OBJECT B
NORAD 64088
BRO-19
NORAD 68422
3.311 12.91 2.4e-07
2026-10-19 11:11:59 BRO-19
NORAD 68422
SL-8 DEB
NORAD 1392
4.476 14.54 9.5e-08
2026-10-19 13:52:43 SPACEMOBILE-004
NORAD 61049
BRO-19
NORAD 68422
4.923 14.34 8.3e-08
2026-10-19 15:27:29 SPACEMOBILE-004
NORAD 61049
BRO-19
NORAD 68422
0.911 14.35 2.4e-06
2026-10-19 15:42:45 S-NET C
NORAD 43189
BRO-19
NORAD 68422
3.313 6.66 3.7e-07
2026-10-20 00:39:22 YAOGAN-36 05B
NORAD 57454
BRO-19
NORAD 68422
0.168 13.16 9.0e-05
2026-10-20 05:04:30 SKYBEE-A01
NORAD 62671
BRO-19
NORAD 68422
4.034 13.04 1.6e-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