View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 65403U 26145.27756272 +.00000000 +00000-0 +63291-3 0 00001
2 65403 97.7734 261.5235 0010991 10.1061 350.0381 14.99783816 06
| Epoch (UTC): | 25 May 2026 06:39:41 |
| Eccentricity: | 0.0010991 |
| inclination: | 97.7734° |
| perigee height: | 560 km |
| apogee height: | 575 km |
| right ascension of ascending node: | 261.5235° |
| argument of perigee: | 10.1061° |
| revolutions per day: | 14.99783816 |
| mean anomaly at epoch: | 350.0381° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|