View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 61204U 26145.43933743 +.00000000 +00000-0 +10424-4 0 00005
2 61204 53.1581 157.8727 0001024 89.0593 271.0542 15.69699920 03
| Epoch (UTC): | 25 May 2026 10:32:38 |
| Eccentricity: | 0.0001024 |
| inclination: | 53.1581° |
| perigee height: | 359 km |
| apogee height: | 360 km |
| right ascension of ascending node: | 157.8727° |
| argument of perigee: | 89.0593° |
| revolutions per day: | 15.69699920 |
| mean anomaly at epoch: | 271.0542° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|