View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 36795U 26109.46620560 +.00000000 +00000-0 +58178-4 0 00003
2 36795 98.0010 160.3736 0011868 27.2764 332.9068 14.78655734 09
| Epoch (UTC): | 19 April 2026 11:11:20 |
| Eccentricity: | 0.0011868 |
| inclination: | 98.0010° |
| perigee height: | 625 km |
| apogee height: | 642 km |
| right ascension of ascending node: | 160.3736° |
| argument of perigee: | 27.2764° |
| revolutions per day: | 14.78655734 |
| mean anomaly at epoch: | 332.9068° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|