View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 52704U 26145.39538870 +.00000000 +00000-0 -32201-5 0 00006
2 52704 53.2114 149.7766 0000998 66.8804 293.2294 15.08843579 05
| Epoch (UTC): | 25 May 2026 09:29:21 |
| Eccentricity: | 0.0000998 |
| inclination: | 53.2114° |
| perigee height: | 539 km |
| apogee height: | 540 km |
| right ascension of ascending node: | 149.7766° |
| argument of perigee: | 66.8804° |
| revolutions per day: | 15.08843579 |
| mean anomaly at epoch: | 293.2294° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|