View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 62293U 26145.59158913 +.00000000 +00000-0 +49709-4 0 00007
2 62293 59.9146 339.4450 0012187 359.9024 0.1980 13.75196272 08
| Epoch (UTC): | 25 May 2026 14:11:53 |
| Eccentricity: | 0.0012187 |
| inclination: | 59.9146° |
| perigee height: | 972 km |
| apogee height: | 990 km |
| right ascension of ascending node: | 339.4450° |
| argument of perigee: | 359.9024° |
| revolutions per day: | 13.75196272 |
| mean anomaly at epoch: | 0.1980° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|