View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 53807U 26065.28981895 +.00000000 +00000-0 +20801-3 0 00009
2 53807 53.2294 156.6061 0005166 209.8583 150.2128 15.37095496 06
| Epoch (UTC): | 06 March 2026 06:57:20 |
| Eccentricity: | 0.0005166 |
| inclination: | 53.2294° |
| perigee height: | 451 km |
| apogee height: | 458 km |
| right ascension of ascending node: | 156.6061° |
| argument of perigee: | 209.8583° |
| revolutions per day: | 15.37095496 |
| mean anomaly at epoch: | 150.2128° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|