View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 23967U 26142.10661080 +.00000000 +00000-0 +00000-0 0 00007
2 23967 11.0923 17.2267 0005495 101.5119 119.7225 1.00222991 04
| Epoch (UTC): | 22 May 2026 02:33:31 |
| Eccentricity: | 0.0005495 |
| inclination: | 11.0923° |
| perigee height: | 35777 km |
| apogee height: | 35823 km |
| right ascension of ascending node: | 17.2267° |
| argument of perigee: | 101.5119° |
| revolutions per day: | 1.00222991 |
| mean anomaly at epoch: | 119.7225° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|