View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 63697U 26145.48992179 +.00000000 +00000-0 +77892-3 0 00007
2 63697 53.1581 221.7293 0001012 45.3972 314.7113 15.34404433 07
| Epoch (UTC): | 25 May 2026 11:45:29 |
| Eccentricity: | 0.0001012 |
| inclination: | 53.1581° |
| perigee height: | 462 km |
| apogee height: | 463 km |
| right ascension of ascending node: | 221.7293° |
| argument of perigee: | 45.3972° |
| revolutions per day: | 15.34404433 |
| mean anomaly at epoch: | 314.7113° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|