View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 40890U 26144.40733509 +.00000000 +00000-0 +00000-0 0 00002
2 40890 54.9514 222.2612 0001728 22.9304 337.1304 1.70474019 00
| Epoch (UTC): | 24 May 2026 09:46:33 |
| Eccentricity: | 0.0001728 |
| inclination: | 54.9514° |
| perigee height: | 23217 km |
| apogee height: | 23227 km |
| right ascension of ascending node: | 222.2612° |
| argument of perigee: | 22.9304° |
| revolutions per day: | 1.70474019 |
| mean anomaly at epoch: | 337.1304° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|