View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 29479U 26114.01908529 +.00000000 +00000-0 +93706-4 0 00001
2 29479 98.0581 130.9662 0018952 99.5895 260.7453 14.68541480 09
| Epoch (UTC): | 24 April 2026 00:27:28 |
| Eccentricity: | 0.0018952 |
| inclination: | 98.0581° |
| perigee height: | 652 km |
| apogee height: | 679 km |
| right ascension of ascending node: | 130.9662° |
| argument of perigee: | 99.5895° |
| revolutions per day: | 14.68541480 |
| mean anomaly at epoch: | 260.7453° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|