View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 24827U 26065.27192197 +.00000000 +00000-0 +48741-3 0 00000
2 24827 63.3106 18.5046 1089392 68.4177 66.8102 11.07979550 00
| Epoch (UTC): | 06 March 2026 06:31:34 |
| Eccentricity: | 0.1089392 |
| inclination: | 63.3106° |
| perigee height: | 1195 km |
| apogee height: | 3047 km |
| right ascension of ascending node: | 18.5046° |
| argument of perigee: | 68.4177° |
| revolutions per day: | 11.07979550 |
| mean anomaly at epoch: | 66.8102° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|