View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 63809U 26145.34670979 +.00000000 +00000-0 +69243-3 0 00009
2 63809 43.0012 100.0386 0001373 262.3124 97.7572 15.27597111 06
| Epoch (UTC): | 25 May 2026 08:19:15 |
| Eccentricity: | 0.0001373 |
| inclination: | 43.0012° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 100.0386° |
| argument of perigee: | 262.3124° |
| revolutions per day: | 15.27597111 |
| mean anomaly at epoch: | 97.7572° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|