View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 40376U 26088.14861493 +.00000000 +00000-0 +14061-3 0 00008
2 40376 98.1308 96.3660 0001852 99.9325 260.2086 14.63363305 02
| Epoch (UTC): | 29 March 2026 03:34:00 |
| Eccentricity: | 0.0001852 |
| inclination: | 98.1308° |
| perigee height: | 681 km |
| apogee height: | 684 km |
| right ascension of ascending node: | 96.3660° |
| argument of perigee: | 99.9325° |
| revolutions per day: | 14.63363305 |
| mean anomaly at epoch: | 260.2086° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|