View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 23608U 26064.72365328 +.00000000 +00000-0 +89658-3 0 00005
2 23608 98.2875 268.3896 0007460 49.6896 310.5002 15.46830303 05
| Epoch (UTC): | 05 March 2026 17:22:03 |
| Eccentricity: | 0.0007460 |
| inclination: | 98.2875° |
| perigee height: | 421 km |
| apogee height: | 431 km |
| right ascension of ascending node: | 268.3896° |
| argument of perigee: | 49.6896° |
| revolutions per day: | 15.46830303 |
| mean anomaly at epoch: | 310.5002° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|