View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 36605U 26152.44920714 +.00000000 +00000-0 +38591-4 0 00000
2 36605 97.4445 160.3804 0001783 80.8335 279.3101 15.19149361 06
| Epoch (UTC): | 01 June 2026 10:46:51 |
| Eccentricity: | 0.0001783 |
| inclination: | 97.4445° |
| perigee height: | 507 km |
| apogee height: | 510 km |
| right ascension of ascending node: | 160.3804° |
| argument of perigee: | 80.8335° |
| revolutions per day: | 15.19149361 |
| mean anomaly at epoch: | 279.3101° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|