View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 29228U 26017.94517551 +.00000000 +00000-0 +13447-3 0 00001
2 29228 69.9322 8.2529 0005527 225.7225 134.3488 15.12387848 04
| Epoch (UTC): | 17 January 2026 22:41:03 |
| Eccentricity: | 0.0005527 |
| inclination: | 69.9322° |
| perigee height: | 525 km |
| apogee height: | 533 km |
| right ascension of ascending node: | 8.2529° |
| argument of perigee: | 225.7225° |
| revolutions per day: | 15.12387848 |
| mean anomaly at epoch: | 134.3488° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|