View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 61773U 26145.58970787 +.00000000 +00000-0 +64587-3 0 00009
2 61773 97.2951 21.1623 0007149 29.5796 330.5863 15.56478062 05
| Epoch (UTC): | 25 May 2026 14:09:10 |
| Eccentricity: | 0.0007149 |
| inclination: | 97.2951° |
| perigee height: | 393 km |
| apogee height: | 403 km |
| right ascension of ascending node: | 21.1623° |
| argument of perigee: | 29.5796° |
| revolutions per day: | 15.56478062 |
| mean anomaly at epoch: | 330.5863° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|