View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 07734U 26053.60614457 +.00000000 +00000-0 +47307-4 0 00008
2 07734 114.9873 326.0791 0016887 308.4318 51.5244 14.19161946 04
| Epoch (UTC): | 22 February 2026 14:32:50 |
| Eccentricity: | 0.0016887 |
| inclination: | 114.9873° |
| perigee height: | 816 km |
| apogee height: | 840 km |
| right ascension of ascending node: | 326.0791° |
| argument of perigee: | 308.4318° |
| revolutions per day: | 14.19161946 |
| mean anomaly at epoch: | 51.5244° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|