View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 40042U 26145.53057890 +.00000000 +00000-0 +54892-3 0 00009
2 40042 98.0964 169.6628 0006385 212.9613 147.1229 15.32350806 01
| Epoch (UTC): | 25 May 2026 12:44:02 |
| Eccentricity: | 0.0006385 |
| inclination: | 98.0964° |
| perigee height: | 464 km |
| apogee height: | 473 km |
| right ascension of ascending node: | 169.6628° |
| argument of perigee: | 212.9613° |
| revolutions per day: | 15.32350806 |
| mean anomaly at epoch: | 147.1229° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|