View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 11511U 26088.22619036 +.00000000 +00000-0 +89826-4 0 00002
2 11511 74.0367 176.5931 0015614 352.3251 7.7662 14.38286374 02
| Epoch (UTC): | 29 March 2026 05:25:42 |
| Eccentricity: | 0.0015614 |
| inclination: | 74.0367° |
| perigee height: | 753 km |
| apogee height: | 775 km |
| right ascension of ascending node: | 176.5931° |
| argument of perigee: | 352.3251° |
| revolutions per day: | 14.38286374 |
| mean anomaly at epoch: | 7.7662° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|