View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 42960U 26145.40118825 +.00000000 +00000-0 +14966-4 0 00001
2 42960 86.3990 34.7951 0002300 78.4005 281.7449 14.34218130 08
| Epoch (UTC): | 25 May 2026 09:37:42 |
| Eccentricity: | 0.0002300 |
| inclination: | 86.3990° |
| perigee height: | 776 km |
| apogee height: | 779 km |
| right ascension of ascending node: | 34.7951° |
| argument of perigee: | 78.4005° |
| revolutions per day: | 14.34218130 |
| mean anomaly at epoch: | 281.7449° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|