View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 15595U 26017.88223111 +.00000000 +00000-0 +93239-4 0 00000
2 15595 108.0438 128.6166 0002346 274.3196 85.7678 14.39862694 01
| Epoch (UTC): | 17 January 2026 21:10:24 |
| Eccentricity: | 0.0002346 |
| inclination: | 108.0438° |
| perigee height: | 757 km |
| apogee height: | 761 km |
| right ascension of ascending node: | 128.6166° |
| argument of perigee: | 274.3196° |
| revolutions per day: | 14.39862694 |
| mean anomaly at epoch: | 85.7678° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|