View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 40908U 26017.99781808 +.00000000 +00000-0 +30986-3 0 00009
2 40908 97.4873 49.5211 0009643 80.6159 279.6180 15.45957040 07
| Epoch (UTC): | 17 January 2026 23:56:51 |
| Eccentricity: | 0.0009643 |
| inclination: | 97.4873° |
| perigee height: | 422 km |
| apogee height: | 435 km |
| right ascension of ascending node: | 49.5211° |
| argument of perigee: | 80.6159° |
| revolutions per day: | 15.45957040 |
| mean anomaly at epoch: | 279.6180° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|