View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 00016U 26134.95283191 +.00000000 +00000-0 +22469-5 0 00002
2 00016 34.2687 41.1605 2018246 340.1616 13.0303 10.49588360 04
| Epoch (UTC): | 14 May 2026 22:52:04 |
| Eccentricity: | 0.2018246 |
| inclination: | 34.2687° |
| perigee height: | 655 km |
| apogee height: | 4212 km |
| right ascension of ascending node: | 41.1605° |
| argument of perigee: | 340.1616° |
| revolutions per day: | 10.49588360 |
| mean anomaly at epoch: | 13.0303° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|