View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 40376U 26067.56710983 +.00000000 +00000-0 +16374-3 0 00007
2 40376 98.1313 76.0713 0001383 112.3789 247.7560 14.63337820 05
| Epoch (UTC): | 08 March 2026 13:36:38 |
| Eccentricity: | 0.0001383 |
| inclination: | 98.1313° |
| perigee height: | 681 km |
| apogee height: | 683 km |
| right ascension of ascending node: | 76.0713° |
| argument of perigee: | 112.3789° |
| revolutions per day: | 14.63337820 |
| mean anomaly at epoch: | 247.7560° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|