View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 59458U 26145.53056882 +.00000000 +00000-0 +12284-3 0 00009
2 59458 43.0066 320.6416 0002687 270.7026 89.3518 15.27567736 04
| Epoch (UTC): | 25 May 2026 12:44:01 |
| Eccentricity: | 0.0002687 |
| inclination: | 43.0066° |
| perigee height: | 481 km |
| apogee height: | 485 km |
| right ascension of ascending node: | 320.6416° |
| argument of perigee: | 270.7026° |
| revolutions per day: | 15.27567736 |
| mean anomaly at epoch: | 89.3518° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|