View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 65358U 26145.45903108 +.00000000 +00000-0 +27685-3 0 00009
2 65358 53.1589 171.2593 0001275 75.3520 284.7622 15.30205215 00
| Epoch (UTC): | 25 May 2026 11:01:00 |
| Eccentricity: | 0.0001275 |
| inclination: | 53.1589° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 171.2593° |
| argument of perigee: | 75.3520° |
| revolutions per day: | 15.30205215 |
| mean anomaly at epoch: | 284.7622° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|