View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 40042U 26053.82031272 +.00000000 +00000-0 +80979-3 0 00000
2 40042 98.1066 69.5812 0007864 172.0896 188.0467 15.28839747 09
| Epoch (UTC): | 22 February 2026 19:41:15 |
| Eccentricity: | 0.0007864 |
| inclination: | 98.1066° |
| perigee height: | 474 km |
| apogee height: | 485 km |
| right ascension of ascending node: | 69.5812° |
| argument of perigee: | 172.0896° |
| revolutions per day: | 15.28839747 |
| mean anomaly at epoch: | 188.0467° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|