View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 64842U 26145.11969338 +.00000000 +00000-0 +16069-3 0 00000
2 64842 97.4509 0.3967 0001863 77.4149 282.7287 15.05656070 06
| Epoch (UTC): | 25 May 2026 02:52:21 |
| Eccentricity: | 0.0001863 |
| inclination: | 97.4509° |
| perigee height: | 548 km |
| apogee height: | 551 km |
| right ascension of ascending node: | 0.3967° |
| argument of perigee: | 77.4149° |
| revolutions per day: | 15.05656070 |
| mean anomaly at epoch: | 282.7287° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|