View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 63650U 26145.42901384 +.00000000 +00000-0 +59305-3 0 00007
2 63650 42.9985 291.7812 0001082 282.6671 77.4060 15.27590490 08
| Epoch (UTC): | 25 May 2026 10:17:46 |
| Eccentricity: | 0.0001082 |
| inclination: | 42.9985° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 291.7812° |
| argument of perigee: | 282.6671° |
| revolutions per day: | 15.27590490 |
| mean anomaly at epoch: | 77.4060° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|