View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 40071U 26088.17085322 +.00000000 +00000-0 +34238-3 0 00000
2 40071 98.3787 45.0723 0007351 161.0959 199.0531 14.89712802 04
| Epoch (UTC): | 29 March 2026 04:06:01 |
| Eccentricity: | 0.0007351 |
| inclination: | 98.3787° |
| perigee height: | 594 km |
| apogee height: | 604 km |
| right ascension of ascending node: | 45.0723° |
| argument of perigee: | 161.0959° |
| revolutions per day: | 14.89712802 |
| mean anomaly at epoch: | 199.0531° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|