View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 00059U 26073.78572000 +.00000000 +00000-0 +66473-4 0 00004
2 00059 28.2488 248.5987 0188976 243.2921 114.8165 13.53164984 03
| Epoch (UTC): | 14 March 2026 18:51:26 |
| Eccentricity: | 0.0188976 |
| inclination: | 28.2488° |
| perigee height: | 920 km |
| apogee height: | 1201 km |
| right ascension of ascending node: | 248.5987° |
| argument of perigee: | 243.2921° |
| revolutions per day: | 13.53164984 |
| mean anomaly at epoch: | 114.8165° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|