View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 67288U 26145.46914994 +.00000000 +00000-0 +21931-3 0 00007
2 67288 97.3927 220.5842 0012983 73.3431 286.9229 15.22875517 08
| Epoch (UTC): | 25 May 2026 11:15:34 |
| Eccentricity: | 0.0012983 |
| inclination: | 97.3927° |
| perigee height: | 488 km |
| apogee height: | 506 km |
| right ascension of ascending node: | 220.5842° |
| argument of perigee: | 73.3431° |
| revolutions per day: | 15.22875517 |
| mean anomaly at epoch: | 286.9229° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|