View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 18586U 26088.22274852 +.00000000 +00000-0 +95248-4 0 00009
2 18586 74.0055 145.6235 0020129 167.8173 192.3472 14.38330659 04
| Epoch (UTC): | 29 March 2026 05:20:45 |
| Eccentricity: | 0.0020129 |
| inclination: | 74.0055° |
| perigee height: | 750 km |
| apogee height: | 778 km |
| right ascension of ascending node: | 145.6235° |
| argument of perigee: | 167.8173° |
| revolutions per day: | 14.38330659 |
| mean anomaly at epoch: | 192.3472° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|