View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 44539U 26145.57642346 +.00000000 +00000-0 +41736-3 0 00007
2 44539 97.5583 294.7580 0007231 104.7170 255.4877 15.40220090 03
| Epoch (UTC): | 25 May 2026 13:50:02 |
| Eccentricity: | 0.0007231 |
| inclination: | 97.5583° |
| perigee height: | 441 km |
| apogee height: | 450 km |
| right ascension of ascending node: | 294.7580° |
| argument of perigee: | 104.7170° |
| revolutions per day: | 15.40220090 |
| mean anomaly at epoch: | 255.4877° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|