View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 63823U 26109.24601476 +.00000000 +00000-0 +47397-3 0 00006
2 63823 43.0033 299.4548 0001128 257.7380 102.3345 15.27585920 04
| Epoch (UTC): | 19 April 2026 05:54:15 |
| Eccentricity: | 0.0001128 |
| inclination: | 43.0033° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 299.4548° |
| argument of perigee: | 257.7380° |
| revolutions per day: | 15.27585920 |
| mean anomaly at epoch: | 102.3345° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|