View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 15354U 84108B 23009.11911933 .32625147 11883-4 18955-3 0 9997
2 15354 56.9750 267.2387 0004240 230.7923 282.7401 16.54292106113839
| Epoch (UTC): | 09 January 2023 02:51:31 |
| Eccentricity: | 0.0004240 |
| inclination: | 56.9750° |
| perigee height: | 125 km |
| apogee height: | 131 km |
| right ascension of ascending node: | 267.2387° |
| argument of perigee: | 230.7923° |
| revolutions per day: | 16.54292106 |
| mean anomaly at epoch: | 282.7401° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|