View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 44930U 26145.61545845 +.00000000 +00000-0 +10076-2 0 00005
2 44930 53.1461 342.3979 0002834 239.9222 120.1509 15.55676421 05
| Epoch (UTC): | 25 May 2026 14:46:15 |
| Eccentricity: | 0.0002834 |
| inclination: | 53.1461° |
| perigee height: | 398 km |
| apogee height: | 402 km |
| right ascension of ascending node: | 342.3979° |
| argument of perigee: | 239.9222° |
| revolutions per day: | 15.55676421 |
| mean anomaly at epoch: | 120.1509° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|