View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 61967U 26145.29798341 +.00000000 +00000-0 +60261-3 0 00001
2 61967 42.9995 100.2886 0001022 263.8917 96.1818 15.27603542 03
| Epoch (UTC): | 25 May 2026 07:09:05 |
| Eccentricity: | 0.0001022 |
| inclination: | 42.9995° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 100.2886° |
| argument of perigee: | 263.8917° |
| revolutions per day: | 15.27603542 |
| mean anomaly at epoch: | 96.1818° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|