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Mandrake 2B

In orbit NORAD 48908 KTGO-9559-9207-1146-9463 United States of America

Falcon 9 Block 5

Carrier rocket

Space Launch Complex 40

Spaceport

1

Observations all time

Mission information
Spacecraft name
Mandrake 2B
Other names
MANDRAKE 2 BAKER
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 40
Launch time
2021-06-30 00:00:00
Separation time
Satellite appearance
Data for the last 30 days
Orbital parameters of the satellite
Perigee
367.63 km
Apogee
369.70 km
Inclination
97.7°
Period
92.0 min
Semi-major axis
6746.8 km
Velocity
7.69 km/s
Orbital elements
TLE source
Celestrak
TLE updated
2026-10-10 12:56:48 UTC
Two-line elements (TLE)
1 48908U 21059AF  26283.12749831  .00034173  00000-0  34186-3 0  9995
2 48908 97.6894 125.8461 0001536 282.9630 77.1458 15.65517774295248
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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 09:23:54 MANDRAKE 2 BAKER
NORAD 48908
FLOCK 4Q-28
NORAD 58280
4.634 12.24 1.4e-07
2026-10-12 10:06:29 MANDRAKE 2 BAKER
NORAD 48908
CZ-2C R/B
NORAD 52794
1.489 14.06 1.0e-06
2026-10-15 07:57:30 MANDRAKE 2 BAKER
NORAD 48908
BANDWAGON-2 OBJECT J
NORAD 62385
3.119 14.30 2.2e-07
2026-10-16 23:40:10 MANDRAKE 2 BAKER
NORAD 48908
USA 62
NORAD 20692
3.497 12.71 2.3e-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