View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 49416U 26145.54672494 +.00000000 +00000-0 -18059-4 0 00004
2 49416 53.2132 244.0952 0001430 83.4327 276.6827 15.08844913 04
| Epoch (UTC): | 25 May 2026 13:07:17 |
| Eccentricity: | 0.0001430 |
| inclination: | 53.2132° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 244.0952° |
| argument of perigee: | 83.4327° |
| revolutions per day: | 15.08844913 |
| mean anomaly at epoch: | 276.6827° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|