View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 59863U 26145.44376674 +.00000000 +00000-0 +57163-4 0 00009
2 59863 43.0006 204.6204 0001062 260.2777 99.7955 15.27584217 00
| Epoch (UTC): | 25 May 2026 10:39:01 |
| Eccentricity: | 0.0001062 |
| inclination: | 43.0006° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 204.6204° |
| argument of perigee: | 260.2777° |
| revolutions per day: | 15.27584217 |
| mean anomaly at epoch: | 99.7955° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|