View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 42692U 26152.51354608 +.00000000 +00000-0 +00000-0 0 00004
2 42692 0.0578 85.5014 0003106 355.9853 278.5538 1.00272257 00
| Epoch (UTC): | 01 June 2026 12:19:30 |
| Eccentricity: | 0.0003106 |
| inclination: | 0.0578° |
| perigee height: | 35773 km |
| apogee height: | 35800 km |
| right ascension of ascending node: | 85.5014° |
| argument of perigee: | 355.9853° |
| revolutions per day: | 1.00272257 |
| mean anomaly at epoch: | 278.5538° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|