View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 00011U 26073.33399362 +.00000000 +00000-0 +47571-3 0 00008
2 00011 32.8743 84.0882 1445783 237.1177 108.2080 11.90277025 04
| Epoch (UTC): | 14 March 2026 08:00:57 |
| Eccentricity: | 0.1445783 |
| inclination: | 32.8743° |
| perigee height: | 553 km |
| apogee height: | 2896 km |
| right ascension of ascending node: | 84.0882° |
| argument of perigee: | 237.1177° |
| revolutions per day: | 11.90277025 |
| mean anomaly at epoch: | 108.2080° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|