View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 59169U 26145.39200685 +.00000000 +00000-0 -78548-4 0 00001
2 59169 43.0003 34.0736 0001103 263.2447 96.8280 15.27579431 05
| Epoch (UTC): | 25 May 2026 09:24:29 |
| Eccentricity: | 0.0001103 |
| inclination: | 43.0003° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 34.0736° |
| argument of perigee: | 263.2447° |
| revolutions per day: | 15.27579431 |
| mean anomaly at epoch: | 96.8280° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|