View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 62765U 26145.51738715 +.00000000 +00000-0 +81758-3 0 00006
2 62765 53.1600 324.9025 0001097 84.1822 275.9305 15.34407835 01
| Epoch (UTC): | 25 May 2026 12:25:02 |
| Eccentricity: | 0.0001097 |
| inclination: | 53.1600° |
| perigee height: | 462 km |
| apogee height: | 463 km |
| right ascension of ascending node: | 324.9025° |
| argument of perigee: | 84.1822° |
| revolutions per day: | 15.34407835 |
| mean anomaly at epoch: | 275.9305° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|