View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 59574U 26145.41839829 +.00000000 +00000-0 +19461-3 0 00009
2 59574 43.0016 296.0088 0001527 269.8630 90.2046 15.27568947 03
| Epoch (UTC): | 25 May 2026 10:02:29 |
| Eccentricity: | 0.0001527 |
| inclination: | 43.0016° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 296.0088° |
| argument of perigee: | 269.8630° |
| revolutions per day: | 15.27568947 |
| mean anomaly at epoch: | 90.2046° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|