View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 62813U 26145.18080933 +.00000000 +00000-0 +53642-3 0 00006
2 62813 53.1603 314.0085 0001644 86.7319 273.3870 15.30211620 01
| Epoch (UTC): | 25 May 2026 04:20:21 |
| Eccentricity: | 0.0001644 |
| inclination: | 53.1603° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 314.0085° |
| argument of perigee: | 86.7319° |
| revolutions per day: | 15.30211620 |
| mean anomaly at epoch: | 273.3870° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|