View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 29228U 26108.14051508 +.00000000 +00000-0 +79087-4 0 00002
2 29228 69.9296 134.9591 0002620 357.5086 2.6067 15.12956140 07
| Epoch (UTC): | 18 April 2026 03:22:20 |
| Eccentricity: | 0.0002620 |
| inclination: | 69.9296° |
| perigee height: | 525 km |
| apogee height: | 529 km |
| right ascension of ascending node: | 134.9591° |
| argument of perigee: | 357.5086° |
| revolutions per day: | 15.12956140 |
| mean anomaly at epoch: | 2.6067° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|