View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 15495U 26104.88037310 +.00000000 +00000-0 +25972-4 0 00009
2 15495 82.5250 44.8237 0020543 122.1741 238.1472 14.86154072 03
| Epoch (UTC): | 14 April 2026 21:07:44 |
| Eccentricity: | 0.0020543 |
| inclination: | 82.5250° |
| perigee height: | 596 km |
| apogee height: | 624 km |
| right ascension of ascending node: | 44.8237° |
| argument of perigee: | 122.1741° |
| revolutions per day: | 14.86154072 |
| mean anomaly at epoch: | 238.1472° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|