View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 65405U 26145.54111402 +.00000000 +00000-0 +10605-2 0 00003
2 65405 53.1561 235.1645 0000591 304.2917 55.8028 15.31712224 06
| Epoch (UTC): | 25 May 2026 12:59:12 |
| Eccentricity: | 0.0000591 |
| inclination: | 53.1561° |
| perigee height: | 470 km |
| apogee height: | 471 km |
| right ascension of ascending node: | 235.1645° |
| argument of perigee: | 304.2917° |
| revolutions per day: | 15.31712224 |
| mean anomaly at epoch: | 55.8028° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|