View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 23608U 26105.56217993 +.00000000 +00000-0 +40262-3 0 00005
2 23608 98.2822 315.1991 0005871 257.2218 102.8375 15.50153042 01
| Epoch (UTC): | 15 April 2026 13:29:32 |
| Eccentricity: | 0.0005871 |
| inclination: | 98.2822° |
| perigee height: | 412 km |
| apogee height: | 420 km |
| right ascension of ascending node: | 315.1991° |
| argument of perigee: | 257.2218° |
| revolutions per day: | 15.50153042 |
| mean anomaly at epoch: | 102.8375° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|