View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 67757U 26145.59048846 +.00000000 +00000-0 +00000-0 0 00007
2 67757 0.3078 296.5763 0000910 231.5852 321.6724 1.00280242 00
| Epoch (UTC): | 25 May 2026 14:10:18 |
| Eccentricity: | 0.0000910 |
| inclination: | 0.3078° |
| perigee height: | 35780 km |
| apogee height: | 35788 km |
| right ascension of ascending node: | 296.5763° |
| argument of perigee: | 231.5852° |
| revolutions per day: | 1.00280242 |
| mean anomaly at epoch: | 321.6724° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|