View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 62238U 26145.59849236 +.00000000 +00000-0 +12583-3 0 00000
2 62238 89.0094 24.8509 0002076 60.6649 299.4709 13.51010328 01
| Epoch (UTC): | 25 May 2026 14:21:49 |
| Eccentricity: | 0.0002076 |
| inclination: | 89.0094° |
| perigee height: | 1067 km |
| apogee height: | 1070 km |
| right ascension of ascending node: | 24.8509° |
| argument of perigee: | 60.6649° |
| revolutions per day: | 13.51010328 |
| mean anomaly at epoch: | 299.4709° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|