View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 15593U 26076.20583347 +.00000000 +00000-0 +46145-4 0 00003
2 15593 82.5385 149.9022 0009521 277.2823 82.7312 14.86824618 02
| Epoch (UTC): | 17 March 2026 04:56:24 |
| Eccentricity: | 0.0009521 |
| inclination: | 82.5385° |
| perigee height: | 601 km |
| apogee height: | 615 km |
| right ascension of ascending node: | 149.9022° |
| argument of perigee: | 277.2823° |
| revolutions per day: | 14.86824618 |
| mean anomaly at epoch: | 82.7312° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|