View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 68728U 26145.58335647 +.00000000 +00000-0 +14301-2 0 00004
2 68728 97.2854 9.2005 0001500 89.1101 163.8573 15.49150090 07
| Epoch (UTC): | 25 May 2026 14:00:01 |
| Eccentricity: | 0.0001500 |
| inclination: | 97.2854° |
| perigee height: | 418 km |
| apogee height: | 420 km |
| right ascension of ascending node: | 9.2005° |
| argument of perigee: | 89.1101° |
| revolutions per day: | 15.49150090 |
| mean anomaly at epoch: | 163.8573° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|