View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 44718U 26145.59448456 +.00000000 +00000-0 +80596-3 0 00001
2 44718 53.1573 176.9629 0002735 34.0026 326.1157 15.47304515 02
| Epoch (UTC): | 25 May 2026 14:16:03 |
| Eccentricity: | 0.0002735 |
| inclination: | 53.1573° |
| perigee height: | 423 km |
| apogee height: | 426 km |
| right ascension of ascending node: | 176.9629° |
| argument of perigee: | 34.0026° |
| revolutions per day: | 15.47304515 |
| mean anomaly at epoch: | 326.1157° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|