View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 23608U 26162.23055903 +.00000000 +00000-0 +56552-3 0 00002
2 23608 98.2744 20.4311 0006965 72.1724 288.0287 15.54397448 00
| Epoch (UTC): | 11 June 2026 05:32:00 |
| Eccentricity: | 0.0006965 |
| inclination: | 98.2744° |
| perigee height: | 399 km |
| apogee height: | 409 km |
| right ascension of ascending node: | 20.4311° |
| argument of perigee: | 72.1724° |
| revolutions per day: | 15.54397448 |
| mean anomaly at epoch: | 288.0287° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|