View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 23467U 26145.50641669 +.00000000 +00000-0 +00000-0 0 00000
2 23467 9.6975 13.3077 0003137 41.9864 182.4045 1.00268825 03
| Epoch (UTC): | 25 May 2026 12:09:14 |
| Eccentricity: | 0.0003137 |
| inclination: | 9.6975° |
| perigee height: | 35774 km |
| apogee height: | 35801 km |
| right ascension of ascending node: | 13.3077° |
| argument of perigee: | 41.9864° |
| revolutions per day: | 1.00268825 |
| mean anomaly at epoch: | 182.4045° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|