View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 40042U 26073.58043193 +.00000000 +00000-0 +10141-2 0 00003
2 40042 98.1050 91.1045 0009577 114.5352 245.6886 15.29795133 08
| Epoch (UTC): | 14 March 2026 13:55:49 |
| Eccentricity: | 0.0009577 |
| inclination: | 98.1050° |
| perigee height: | 470 km |
| apogee height: | 483 km |
| right ascension of ascending node: | 91.1045° |
| argument of perigee: | 114.5352° |
| revolutions per day: | 15.29795133 |
| mean anomaly at epoch: | 245.6886° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|