View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 40016U 26032.37618336 +.00000000 +00000-0 +16022-3 0 00008
2 40016 97.7346 183.3949 0045593 153.9370 206.4151 14.79305143 06
| Epoch (UTC): | 01 February 2026 09:01:42 |
| Eccentricity: | 0.0045593 |
| inclination: | 97.7346° |
| perigee height: | 600 km |
| apogee height: | 663 km |
| right ascension of ascending node: | 183.3949° |
| argument of perigee: | 153.9370° |
| revolutions per day: | 14.79305143 |
| mean anomaly at epoch: | 206.4151° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|