View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 62668U 26145.44042924 +.00000000 +00000-0 +14752-3 0 00000
2 62668 97.3962 224.7332 0005897 69.4930 290.6939 15.22175435 02
| Epoch (UTC): | 25 May 2026 10:34:13 |
| Eccentricity: | 0.0005897 |
| inclination: | 97.3962° |
| perigee height: | 495 km |
| apogee height: | 503 km |
| right ascension of ascending node: | 224.7332° |
| argument of perigee: | 69.4930° |
| revolutions per day: | 15.22175435 |
| mean anomaly at epoch: | 290.6939° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|