View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 62259U 26160.64016946 +.00000000 +00000-0 +00000-0 0 00008
2 62259 0.0165 322.5469 0004800 351.5357 89.2433 1.00270739 08
| Epoch (UTC): | 09 June 2026 15:21:50 |
| Eccentricity: | 0.0004800 |
| inclination: | 0.0165° |
| perigee height: | 35767 km |
| apogee height: | 35807 km |
| right ascension of ascending node: | 322.5469° |
| argument of perigee: | 351.5357° |
| revolutions per day: | 1.00270739 |
| mean anomaly at epoch: | 89.2433° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|