View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 65806U 26145.34324002 +.00000000 +00000-0 +68637-3 0 00007
2 65806 97.4498 8.1226 0002025 80.9691 279.1766 15.05654073 03
| Epoch (UTC): | 25 May 2026 08:14:15 |
| Eccentricity: | 0.0002025 |
| inclination: | 97.4498° |
| perigee height: | 548 km |
| apogee height: | 551 km |
| right ascension of ascending node: | 8.1226° |
| argument of perigee: | 80.9691° |
| revolutions per day: | 15.05654073 |
| mean anomaly at epoch: | 279.1766° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|