View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 14064U 26073.53768998 +.00000000 +00000-0 +97126-3 0 00009
2 14064 64.9903 4.2926 0052387 226.3352 133.3437 15.35288430 02
| Epoch (UTC): | 14 March 2026 12:54:16 |
| Eccentricity: | 0.0052387 |
| inclination: | 64.9903° |
| perigee height: | 424 km |
| apogee height: | 496 km |
| right ascension of ascending node: | 4.2926° |
| argument of perigee: | 226.3352° |
| revolutions per day: | 15.35288430 |
| mean anomaly at epoch: | 133.3437° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|