View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 31114U 26160.24014388 +.00000000 +00000-0 +53224-4 0 00008
2 31114 98.4091 268.9801 0059475 29.1128 331.3344 14.20274415 01
| Epoch (UTC): | 09 June 2026 05:45:48 |
| Eccentricity: | 0.0059475 |
| inclination: | 98.4091° |
| perigee height: | 782 km |
| apogee height: | 867 km |
| right ascension of ascending node: | 268.9801° |
| argument of perigee: | 29.1128° |
| revolutions per day: | 14.20274415 |
| mean anomaly at epoch: | 331.3344° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|