View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 67781U 26145.58335647 +.00000000 +00000-0 +22914-2 0 00001
2 67781 51.8850 208.8223 0009457 345.1624 315.0008 15.26043023 06
| Epoch (UTC): | 25 May 2026 14:00:01 |
| Eccentricity: | 0.0009457 |
| inclination: | 51.8850° |
| perigee height: | 481 km |
| apogee height: | 494 km |
| right ascension of ascending node: | 208.8223° |
| argument of perigee: | 345.1624° |
| revolutions per day: | 15.26043023 |
| mean anomaly at epoch: | 315.0008° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|