View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 68703U 26145.58335647 +.00000000 +00000-0 -46562-1 0 00001
2 68703 53.1591 37.2522 0001447 118.0982 149.5774 15.42224610 00
| Epoch (UTC): | 25 May 2026 14:00:01 |
| Eccentricity: | 0.0001447 |
| inclination: | 53.1591° |
| perigee height: | 439 km |
| apogee height: | 441 km |
| right ascension of ascending node: | 37.2522° |
| argument of perigee: | 118.0982° |
| revolutions per day: | 15.42224610 |
| mean anomaly at epoch: | 149.5774° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|