View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 59581U 26145.11957816 +.00000000 +00000-0 +46503-4 0 00009
2 59581 43.0023 297.1859 0001478 273.5679 86.5003 15.27569322 06
| Epoch (UTC): | 25 May 2026 02:52:11 |
| Eccentricity: | 0.0001478 |
| inclination: | 43.0023° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 297.1859° |
| argument of perigee: | 273.5679° |
| revolutions per day: | 15.27569322 |
| mean anomaly at epoch: | 86.5003° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|