View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 59404U 26145.42004647 +.00000000 +00000-0 +51703-3 0 00009
2 59404 43.0012 291.7810 0001656 263.1618 96.9045 15.27552770 01
| Epoch (UTC): | 25 May 2026 10:04:52 |
| Eccentricity: | 0.0001656 |
| inclination: | 43.0012° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 291.7810° |
| argument of perigee: | 263.1618° |
| revolutions per day: | 15.27552770 |
| mean anomaly at epoch: | 96.9045° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|