View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 59470U 26145.51307367 +.00000000 +00000-0 +14040-3 0 00000
2 59470 43.0015 317.0465 0001225 275.5357 84.5355 15.27589709 03
| Epoch (UTC): | 25 May 2026 12:18:49 |
| Eccentricity: | 0.0001225 |
| inclination: | 43.0015° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 317.0465° |
| argument of perigee: | 275.5357° |
| revolutions per day: | 15.27589709 |
| mean anomaly at epoch: | 84.5355° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|