View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 68120U 26145.40864196 +.00000000 +00000-0 +91186-3 0 00004
2 68120 97.2837 106.0853 0002102 97.8646 262.2836 15.33486763 08
| Epoch (UTC): | 25 May 2026 09:48:26 |
| Eccentricity: | 0.0002102 |
| inclination: | 97.2837° |
| perigee height: | 464 km |
| apogee height: | 467 km |
| right ascension of ascending node: | 106.0853° |
| argument of perigee: | 97.8646° |
| revolutions per day: | 15.33486763 |
| mean anomaly at epoch: | 262.2836° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|