View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 61515U 26145.30494833 +.00000000 +00000-0 +22333-4 0 00000
2 61515 53.1601 146.5112 0001114 92.1240 267.9889 15.31701860 02
| Epoch (UTC): | 25 May 2026 07:19:07 |
| Eccentricity: | 0.0001114 |
| inclination: | 53.1601° |
| perigee height: | 470 km |
| apogee height: | 471 km |
| right ascension of ascending node: | 146.5112° |
| argument of perigee: | 92.1240° |
| revolutions per day: | 15.31701860 |
| mean anomaly at epoch: | 267.9889° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|