View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 37886U 26087.84034071 +.00000000 +00000-0 +73864-4 0 00007
2 37886 74.0258 295.8487 0024474 299.2295 60.6412 14.39748245 08
| Epoch (UTC): | 28 March 2026 20:10:05 |
| Eccentricity: | 0.0024474 |
| inclination: | 74.0258° |
| perigee height: | 742 km |
| apogee height: | 777 km |
| right ascension of ascending node: | 295.8487° |
| argument of perigee: | 299.2295° |
| revolutions per day: | 14.39748245 |
| mean anomaly at epoch: | 60.6412° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|