View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 65550U 26145.44032429 +.00000000 +00000-0 +18991-3 0 00001
2 65550 49.9905 145.1340 0003855 316.2262 43.8370 14.84083827 00
| Epoch (UTC): | 25 May 2026 10:34:04 |
| Eccentricity: | 0.0003855 |
| inclination: | 49.9905° |
| perigee height: | 614 km |
| apogee height: | 619 km |
| right ascension of ascending node: | 145.1340° |
| argument of perigee: | 316.2262° |
| revolutions per day: | 14.84083827 |
| mean anomaly at epoch: | 43.8370° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|