View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 68049U 26145.12732273 +.00000000 +00000-0 +11234-2 0 00008
2 68049 53.1587 53.2556 0001162 107.0454 253.0678 15.38825278 05
| Epoch (UTC): | 25 May 2026 03:03:20 |
| Eccentricity: | 0.0001162 |
| inclination: | 53.1587° |
| perigee height: | 449 km |
| apogee height: | 450 km |
| right ascension of ascending node: | 53.2556° |
| argument of perigee: | 107.0454° |
| revolutions per day: | 15.38825278 |
| mean anomaly at epoch: | 253.0678° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|