View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 40057U 26073.23762456 +.00000000 +00000-0 +55638-3 0 00002
2 40057 98.2616 332.8888 0006500 221.6091 138.4635 14.96922309 07
| Epoch (UTC): | 14 March 2026 05:42:10 |
| Eccentricity: | 0.0006500 |
| inclination: | 98.2616° |
| perigee height: | 572 km |
| apogee height: | 581 km |
| right ascension of ascending node: | 332.8888° |
| argument of perigee: | 221.6091° |
| revolutions per day: | 14.96922309 |
| mean anomaly at epoch: | 138.4635° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|