View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 14064U 26064.15601376 +.00000000 +00000-0 +79686-3 0 00004
2 14064 64.9895 35.2442 0053620 229.7383 129.9058 15.34764388 01
| Epoch (UTC): | 05 March 2026 03:44:39 |
| Eccentricity: | 0.0053620 |
| inclination: | 64.9895° |
| perigee height: | 425 km |
| apogee height: | 498 km |
| right ascension of ascending node: | 35.2442° |
| argument of perigee: | 229.7383° |
| revolutions per day: | 15.34764388 |
| mean anomaly at epoch: | 129.9058° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|