View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 40076U 26032.50351468 +.00000000 +00000-0 +54382-3 0 00000
2 40076 98.3717 11.6052 0007313 22.0971 338.0570 15.10697048 01
| Epoch (UTC): | 01 February 2026 12:05:03 |
| Eccentricity: | 0.0007313 |
| inclination: | 98.3717° |
| perigee height: | 529 km |
| apogee height: | 539 km |
| right ascension of ascending node: | 11.6052° |
| argument of perigee: | 22.0971° |
| revolutions per day: | 15.10697048 |
| mean anomaly at epoch: | 338.0570° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|