View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 53807U 26161.03268586 +.00000000 +00000-0 +16814-3 0 00003
2 53807 53.2293 67.5573 0006861 140.7558 219.3945 15.38180975 03
| Epoch (UTC): | 10 June 2026 00:47:04 |
| Eccentricity: | 0.0006861 |
| inclination: | 53.2293° |
| perigee height: | 447 km |
| apogee height: | 456 km |
| right ascension of ascending node: | 67.5573° |
| argument of perigee: | 140.7558° |
| revolutions per day: | 15.38180975 |
| mean anomaly at epoch: | 219.3945° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|