View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 65443U 26145.30387110 +.00000000 +00000-0 +23719-3 0 00001
2 65443 97.4517 359.4915 0002062 86.0830 274.0633 15.05657971 09
| Epoch (UTC): | 25 May 2026 07:17:34 |
| Eccentricity: | 0.0002062 |
| inclination: | 97.4517° |
| perigee height: | 548 km |
| apogee height: | 551 km |
| right ascension of ascending node: | 359.4915° |
| argument of perigee: | 86.0830° |
| revolutions per day: | 15.05657971 |
| mean anomaly at epoch: | 274.0633° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|