View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 65513U 26145.65362058 +.00000000 +00000-0 +51435-3 0 00007
2 65513 53.1577 272.7948 0002823 105.7262 254.4053 15.34400780 02
| Epoch (UTC): | 25 May 2026 15:41:12 |
| Eccentricity: | 0.0002823 |
| inclination: | 53.1577° |
| perigee height: | 461 km |
| apogee height: | 465 km |
| right ascension of ascending node: | 272.7948° |
| argument of perigee: | 105.7262° |
| revolutions per day: | 15.34400780 |
| mean anomaly at epoch: | 254.4053° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|