View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 63419U 26145.10739194 +.00000000 +00000-0 +74165-3 0 00004
2 63419 43.0014 35.7491 0001376 259.7809 100.2887 15.27601156 03
| Epoch (UTC): | 25 May 2026 02:34:38 |
| Eccentricity: | 0.0001376 |
| inclination: | 43.0014° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 35.7491° |
| argument of perigee: | 259.7809° |
| revolutions per day: | 15.27601156 |
| mean anomaly at epoch: | 100.2887° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|