View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 24279U 26088.09252365 +.00000000 +00000-0 +13419-3 0 00004
2 24279 98.7522 35.9397 0299957 28.5597 343.0995 13.47475384 01
| Epoch (UTC): | 29 March 2026 02:13:14 |
| Eccentricity: | 0.0299957 |
| inclination: | 98.7522° |
| perigee height: | 858 km |
| apogee height: | 1305 km |
| right ascension of ascending node: | 35.9397° |
| argument of perigee: | 28.5597° |
| revolutions per day: | 13.47475384 |
| mean anomaly at epoch: | 343.0995° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|