View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 27942U 26150.46418597 +.00000000 +00000-0 +16081-3 0 00004
2 27942 98.0808 339.3182 0052244 261.5529 97.9762 14.86981210 05
| Epoch (UTC): | 30 May 2026 11:08:25 |
| Eccentricity: | 0.0052244 |
| inclination: | 98.0808° |
| perigee height: | 571 km |
| apogee height: | 644 km |
| right ascension of ascending node: | 339.3182° |
| argument of perigee: | 261.5529° |
| revolutions per day: | 14.86981210 |
| mean anomaly at epoch: | 97.9762° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|