View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 14781U 26070.88900417 +.00000000 +00000-0 +14935-3 0 00001
2 14781 97.7946 37.6292 0008558 137.3196 222.8688 14.90514928 09
| Epoch (UTC): | 11 March 2026 21:20:09 |
| Eccentricity: | 0.0008558 |
| inclination: | 97.7946° |
| perigee height: | 590 km |
| apogee height: | 602 km |
| right ascension of ascending node: | 37.6292° |
| argument of perigee: | 137.3196° |
| revolutions per day: | 14.90514928 |
| mean anomaly at epoch: | 222.8688° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|