View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 61854U 26145.34484962 +.00000000 +00000-0 -63868-4 0 00001
2 61854 43.0012 164.8585 0000983 263.2312 96.8427 15.27583787 01
| Epoch (UTC): | 25 May 2026 08:16:35 |
| Eccentricity: | 0.0000983 |
| inclination: | 43.0012° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 164.8585° |
| argument of perigee: | 263.2312° |
| revolutions per day: | 15.27583787 |
| mean anomaly at epoch: | 96.8427° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|