View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 27042U 26108.19115153 +.00000000 +00000-0 -31720-2 0 00007
2 27042 8.0537 285.8674 7120214 29.1523 95.8697 2.25346227 06
| Epoch (UTC): | 18 April 2026 04:35:15 |
| Eccentricity: | 0.7120214 |
| inclination: | 8.0537° |
| perigee height: | 699 km |
| apogee height: | 35696 km |
| right ascension of ascending node: | 285.8674° |
| argument of perigee: | 29.1523° |
| revolutions per day: | 2.25346227 |
| mean anomaly at epoch: | 95.8697° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|