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BANDWAGON-2 OBJECT V

In orbit NORAD 62396 KERK-9945-2983-3968-7332

Observations 0
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Falcon 9 Block 5 | Bandwagon 2 (Dedicated Mid-Inclination Rideshare)

Falcon 9 Block 5

Carrier rocket

Space Launch Complex 4E

Spaceport

0

Observations all time

Mission information
Spacecraft name
BANDWAGON-2 OBJECT V
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 | Bandwagon 2 (Dedicated Mid-Inclination 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
370.50 km
Apogee
380.68 km
Inclination
45.0°
Period
92.0 min
Semi-major axis
6753.7 km
Velocity
7.7 km/s
Orbital elements
TLE source
Celestrak
TLE updated
2026-10-10 04:46:19 UTC
Two-line elements (TLE)
1 62396U 24247V   26282.79602787  .00102792  00000-0  10201-2 0  9998
2 62396  44.9894 314.1826 0007537  16.7099 343.4046 15.64750904101350
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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 11:17:47 ICEYE-X25
NORAD 56963 		BANDWAGON-2 OBJECT V
NORAD 62396 		4.941 14.43 8.4e-08
2026-10-17 07:53:54 STARLINK-11271
NORAD 60915 		BANDWAGON-2 OBJECT V
NORAD 62396 		4.877 11.29 4.1e-06

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