View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 55047U 26145.61084583 +.00000000 +00000-0 +33273-3 0 00008
2 55047 97.3087 206.9707 0008295 121.6957 238.5092 15.27329301 05
| Epoch (UTC): | 25 May 2026 14:39:37 |
| Eccentricity: | 0.0008295 |
| inclination: | 97.3087° |
| perigee height: | 478 km |
| apogee height: | 489 km |
| right ascension of ascending node: | 206.9707° |
| argument of perigee: | 121.6957° |
| revolutions per day: | 15.27329301 |
| mean anomaly at epoch: | 238.5092° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|