View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 47367U 26145.49454020 +.00000000 +00000-0 +51383-4 0 00000
2 47367 53.1603 65.4442 0001764 88.3376 271.7828 15.31705550 02
| Epoch (UTC): | 25 May 2026 11:52:08 |
| Eccentricity: | 0.0001764 |
| inclination: | 53.1603° |
| perigee height: | 470 km |
| apogee height: | 472 km |
| right ascension of ascending node: | 65.4442° |
| argument of perigee: | 88.3376° |
| revolutions per day: | 15.31705550 |
| mean anomaly at epoch: | 271.7828° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|