View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 29048U 26106.94520322 +.00000000 +00000-0 +10203-3 0 00007
2 29048 71.9676 345.3922 0043422 304.8921 54.8139 14.31342025 06
| Epoch (UTC): | 16 April 2026 22:41:05 |
| Eccentricity: | 0.0043422 |
| inclination: | 71.9676° |
| perigee height: | 756 km |
| apogee height: | 818 km |
| right ascension of ascending node: | 345.3922° |
| argument of perigee: | 304.8921° |
| revolutions per day: | 14.31342025 |
| mean anomaly at epoch: | 54.8139° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|