View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 56457U 26145.18368991 +.00000000 +00000-0 -82497-4 0 00008
2 56457 69.9989 311.6038 0002448 270.7464 89.3414 14.98322442 07
| Epoch (UTC): | 25 May 2026 04:24:30 |
| Eccentricity: | 0.0002448 |
| inclination: | 69.9989° |
| perigee height: | 570 km |
| apogee height: | 574 km |
| right ascension of ascending node: | 311.6038° |
| argument of perigee: | 270.7464° |
| revolutions per day: | 14.98322442 |
| mean anomaly at epoch: | 89.3414° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|