View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 59785U 26145.24771726 +.00000000 +00000-0 +16978-4 0 00006
2 59785 43.0013 133.1059 0001285 269.0806 90.9899 15.27577501 00
| Epoch (UTC): | 25 May 2026 05:56:42 |
| Eccentricity: | 0.0001285 |
| inclination: | 43.0013° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 133.1059° |
| argument of perigee: | 269.0806° |
| revolutions per day: | 15.27577501 |
| mean anomaly at epoch: | 90.9899° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|