View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 00933U 26088.09240175 +.00000000 +00000-0 +80999-3 0 00008
2 00933 81.3364 213.3306 1050985 181.4614 178.3354 12.82366910 02
| Epoch (UTC): | 29 March 2026 02:13:03 |
| Eccentricity: | 0.1050985 |
| inclination: | 81.3364° |
| perigee height: | 522 km |
| apogee height: | 2142 km |
| right ascension of ascending node: | 213.3306° |
| argument of perigee: | 181.4614° |
| revolutions per day: | 12.82366910 |
| mean anomaly at epoch: | 178.3354° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|