View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 16182U 26074.58251279 +.00000000 +00000-0 +57477-4 0 00003
2 16182 71.0017 128.1487 0009742 252.5025 257.8190 14.16598305 04
| Epoch (UTC): | 15 March 2026 13:58:49 |
| Eccentricity: | 0.0009742 |
| inclination: | 71.0017° |
| perigee height: | 830 km |
| apogee height: | 844 km |
| right ascension of ascending node: | 128.1487° |
| argument of perigee: | 252.5025° |
| revolutions per day: | 14.16598305 |
| mean anomaly at epoch: | 257.8190° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|