View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 62516U 26145.54999311 +.00000000 +00000-0 +19309-2 0 00006
2 62516 42.9982 327.7097 0001515 260.9670 99.1026 15.70922619 02
| Epoch (UTC): | 25 May 2026 13:11:59 |
| Eccentricity: | 0.0001515 |
| inclination: | 42.9982° |
| perigee height: | 355 km |
| apogee height: | 357 km |
| right ascension of ascending node: | 327.7097° |
| argument of perigee: | 260.9670° |
| revolutions per day: | 15.70922619 |
| mean anomaly at epoch: | 99.1026° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|