View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 15333U 26076.21072814 +.00000000 +00000-0 +13914-3 0 00005
2 15333 71.0242 240.5985 0018742 16.5702 343.6029 14.14503204 00
| Epoch (UTC): | 17 March 2026 05:03:26 |
| Eccentricity: | 0.0018742 |
| inclination: | 71.0242° |
| perigee height: | 830 km |
| apogee height: | 858 km |
| right ascension of ascending node: | 240.5985° |
| argument of perigee: | 16.5702° |
| revolutions per day: | 14.14503204 |
| mean anomaly at epoch: | 343.6029° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|