View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 16908U 26145.67185420 +.00000000 +00000-0 +24589-4 0 00000
2 16908 50.0078 216.6308 0011349 123.4901 45.9423 12.44516431 08
| Epoch (UTC): | 25 May 2026 16:07:28 |
| Eccentricity: | 0.0011349 |
| inclination: | 50.0078° |
| perigee height: | 1479 km |
| apogee height: | 1496 km |
| right ascension of ascending node: | 216.6308° |
| argument of perigee: | 123.4901° |
| revolutions per day: | 12.44516431 |
| mean anomaly at epoch: | 45.9423° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|