View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 24278U 26075.89203095 +.00000000 +00000-0 +62012-4 0 00007
2 24278 98.5371 297.3369 0349515 336.0816 22.4418 13.53269310 05
| Epoch (UTC): | 16 March 2026 21:24:31 |
| Eccentricity: | 0.0349515 |
| inclination: | 98.5371° |
| perigee height: | 800 km |
| apogee height: | 1320 km |
| right ascension of ascending node: | 297.3369° |
| argument of perigee: | 336.0816° |
| revolutions per day: | 13.53269310 |
| mean anomaly at epoch: | 22.4418° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|