View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 52365U 26145.43264441 +.00000000 +00000-0 +19777-4 0 00005
2 52365 53.2136 204.6067 0000988 85.1138 274.9967 15.08841861 05
| Epoch (UTC): | 25 May 2026 10:23:00 |
| Eccentricity: | 0.0000988 |
| inclination: | 53.2136° |
| perigee height: | 539 km |
| apogee height: | 540 km |
| right ascension of ascending node: | 204.6067° |
| argument of perigee: | 85.1138° |
| revolutions per day: | 15.08841861 |
| mean anomaly at epoch: | 274.9967° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|