View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 63759U 26145.47697557 +.00000000 +00000-0 +11906-2 0 00000
2 63759 43.0021 189.2572 0002127 263.8742 96.1883 15.70862686 04
| Epoch (UTC): | 25 May 2026 11:26:50 |
| Eccentricity: | 0.0002127 |
| inclination: | 43.0021° |
| perigee height: | 355 km |
| apogee height: | 358 km |
| right ascension of ascending node: | 189.2572° |
| argument of perigee: | 263.8742° |
| revolutions per day: | 15.70862686 |
| mean anomaly at epoch: | 96.1883° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|