View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 00115U 26105.20994508 +.00000000 +00000-0 +14736-3 0 00005
2 00115 48.1631 50.6203 0026679 333.8182 26.1387 14.97850525 09
| Epoch (UTC): | 15 April 2026 05:02:19 |
| Eccentricity: | 0.0026679 |
| inclination: | 48.1631° |
| perigee height: | 555 km |
| apogee height: | 592 km |
| right ascension of ascending node: | 50.6203° |
| argument of perigee: | 333.8182° |
| revolutions per day: | 14.97850525 |
| mean anomaly at epoch: | 26.1387° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|