View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 15032U 26110.94749863 +.00000000 +00000-0 +17744-4 0 00001
2 15032 74.0675 288.1700 0016959 352.5864 7.5036 14.36124453 05
| Epoch (UTC): | 20 April 2026 22:44:23 |
| Eccentricity: | 0.0016959 |
| inclination: | 74.0675° |
| perigee height: | 759 km |
| apogee height: | 783 km |
| right ascension of ascending node: | 288.1700° |
| argument of perigee: | 352.5864° |
| revolutions per day: | 14.36124453 |
| mean anomaly at epoch: | 7.5036° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|