View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 42842U 26041.98988468 +.00000000 +00000-0 +74110-3 0 00002
2 42842 97.3789 224.7616 0007635 101.9588 258.2507 15.25859664 06
| Epoch (UTC): | 10 February 2026 23:45:26 |
| Eccentricity: | 0.0007635 |
| inclination: | 97.3789° |
| perigee height: | 483 km |
| apogee height: | 493 km |
| right ascension of ascending node: | 224.7616° |
| argument of perigee: | 101.9588° |
| revolutions per day: | 15.25859664 |
| mean anomaly at epoch: | 258.2507° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|