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Buccaneer MM

In orbit NORAD 63245 BDVO-4886-9138-3275-1637 Australia

Falcon 9

Carrier rocket

База Вандерберг

Spaceport

170

Observations all time

Mission information
Spacecraft name
Buccaneer MM
Other names
Buccaneer Main Mission
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
Spaceport
База Вандерберг
Launch time
2025-03-15 06:43:00
Separation time
Last observers
Observer
Time of receipt
2025-03-18 06:50:48 UTC
Satellite appearance
Data for the last 30 days
Orbital parameters of the satellite
Perigee
576.22 km
Apogee
581.56 km
Inclination
97.7°
Period
96.3 min
Semi-major axis
6957.0 km
Velocity
7.57 km/s
Orbital elements
TLE source
Celestrak
TLE updated
2026-10-10 12:56:50 UTC
Two-line elements (TLE)
1 63245U 25052AM  26283.29347907  .00002391  00000-0  22296-3 0  9995
2 63245 97.6687 171.8783 0003841 167.6404 192.4912 14.95159065 85796
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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 04:55:30 TIMED
NORAD 26998
BUCCANEER MM
NORAD 63245
0.981 15.04 1.6e-06
2026-10-11 05:43:42 TIMED
NORAD 26998
BUCCANEER MM
NORAD 63245
3.213 15.06 1.5e-07
2026-10-11 07:45:48 BUCCANEER MM
NORAD 63245
THOR ABLESTAR DEB
NORAD 548
2.233 14.93 3.3e-07
2026-10-11 10:28:09 BUCCANEER MM
NORAD 63245
TRACERS 1
NORAD 64870
1.353 14.97 8.7e-07
2026-10-12 05:44:34 BUCCANEER MM
NORAD 63245
TRACERS 2
NORAD 64873
3.790 14.97 1.1e-07
2026-10-12 08:45:53 BUCCANEER MM
NORAD 63245
ARIANE 6 R/B
NORAD 60239
2.366 4.81 7.5e-07
2026-10-12 12:22:10 BUCCANEER MM
NORAD 63245
FENGYUN 1C DEB
NORAD 32331
4.731 13.54 1.1e-07
2026-10-12 22:47:03 TIANPING 2A
NORAD 52153
BUCCANEER MM
NORAD 63245
3.305 14.31 1.8e-07
2026-10-13 04:32:47 BUCCANEER MM
NORAD 63245
NOAA 16 DEB
NORAD 42357
4.754 10.25 1.5e-07
2026-10-14 00:48:08 BUCCANEER MM
NORAD 63245
CZ-6A DEB
NORAD 54927
3.320 14.87 1.5e-07
2026-10-16 12:05:47 BUCCANEER MM
NORAD 63245
LEMUR-2-HUBBLE-4
NORAD 64565
2.301 13.87 4.2e-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