View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 31598U 26065.65563858 +.00000000 +00000-0 +41847-3 0 00001
2 31598 97.8863 256.6635 0000944 98.9581 261.1747 14.96505895 09
| Epoch (UTC): | 06 March 2026 15:44:07 |
| Eccentricity: | 0.0000944 |
| inclination: | 97.8863° |
| perigee height: | 577 km |
| apogee height: | 578 km |
| right ascension of ascending node: | 256.6635° |
| argument of perigee: | 98.9581° |
| revolutions per day: | 14.96505895 |
| mean anomaly at epoch: | 261.1747° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|