View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 62365U 26145.60182061 +.00000000 +00000-0 +12119-3 0 00004
2 62365 44.9843 62.5245 0008481 274.9432 85.0432 13.99198595 03
| Epoch (UTC): | 25 May 2026 14:26:37 |
| Eccentricity: | 0.0008481 |
| inclination: | 44.9843° |
| perigee height: | 890 km |
| apogee height: | 903 km |
| right ascension of ascending node: | 62.5245° |
| argument of perigee: | 274.9432° |
| revolutions per day: | 13.99198595 |
| mean anomaly at epoch: | 85.0432° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|