View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 15595U 26088.18870705 +.00000000 +00000-0 +12056-3 0 00005
2 15595 108.0515 274.9419 0002243 255.6333 104.4560 14.39926995 08
| Epoch (UTC): | 29 March 2026 04:31:44 |
| Eccentricity: | 0.0002243 |
| inclination: | 108.0515° |
| perigee height: | 757 km |
| apogee height: | 760 km |
| right ascension of ascending node: | 274.9419° |
| argument of perigee: | 255.6333° |
| revolutions per day: | 14.39926995 |
| mean anomaly at epoch: | 104.4560° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|