View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 11081U 26088.09833095 +.00000000 +00000-0 +70969-4 0 00000
2 11081 99.4133 22.8141 0029197 13.0576 347.1329 13.86101315 08
| Epoch (UTC): | 29 March 2026 02:21:35 |
| Eccentricity: | 0.0029197 |
| inclination: | 99.4133° |
| perigee height: | 921 km |
| apogee height: | 964 km |
| right ascension of ascending node: | 22.8141° |
| argument of perigee: | 13.0576° |
| revolutions per day: | 13.86101315 |
| mean anomaly at epoch: | 347.1329° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|