View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 44310U 26145.59111566 +.00000000 +00000-0 +31865-3 0 00003
2 44310 44.9699 180.2934 0007078 119.9090 240.2496 15.27748976 06
| Epoch (UTC): | 25 May 2026 14:11:12 |
| Eccentricity: | 0.0007078 |
| inclination: | 44.9699° |
| perigee height: | 478 km |
| apogee height: | 487 km |
| right ascension of ascending node: | 180.2934° |
| argument of perigee: | 119.9090° |
| revolutions per day: | 15.27748976 |
| mean anomaly at epoch: | 240.2496° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|