View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 53961U 26145.05871568 +.00000000 +00000-0 +00000-0 0 00005
2 53961 0.0265 29.4982 0001194 11.0489 92.2447 1.00271305 08
| Epoch (UTC): | 25 May 2026 01:24:33 |
| Eccentricity: | 0.0001194 |
| inclination: | 0.0265° |
| perigee height: | 35782 km |
| apogee height: | 35792 km |
| right ascension of ascending node: | 29.4982° |
| argument of perigee: | 11.0489° |
| revolutions per day: | 1.00271305 |
| mean anomaly at epoch: | 92.2447° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|