View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 16182U 26073.59431058 +.00000000 +00000-0 +22353-4 0 00003
2 16182 71.0018 130.2292 0009770 253.6938 258.5487 14.16598173 09
| Epoch (UTC): | 14 March 2026 14:15:48 |
| Eccentricity: | 0.0009770 |
| inclination: | 71.0018° |
| perigee height: | 830 km |
| apogee height: | 844 km |
| right ascension of ascending node: | 130.2292° |
| argument of perigee: | 253.6938° |
| revolutions per day: | 14.16598173 |
| mean anomaly at epoch: | 258.5487° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|