View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 68743U 26145.58335647 +.00000000 +00000-0 -33993-1 0 00009
2 68743 97.2853 9.3107 0002179 83.7000 59.8840 15.52094225 00
| Epoch (UTC): | 25 May 2026 14:00:01 |
| Eccentricity: | 0.0002179 |
| inclination: | 97.2853° |
| perigee height: | 409 km |
| apogee height: | 412 km |
| right ascension of ascending node: | 9.3107° |
| argument of perigee: | 83.7000° |
| revolutions per day: | 15.52094225 |
| mean anomaly at epoch: | 59.8840° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|