View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 47898U 26145.37744950 +.00000000 +00000-0 +10096-3 0 00005
2 47898 53.1583 271.4099 0001914 73.7769 286.3442 15.31711070 04
| Epoch (UTC): | 25 May 2026 09:03:31 |
| Eccentricity: | 0.0001914 |
| inclination: | 53.1583° |
| perigee height: | 469 km |
| apogee height: | 472 km |
| right ascension of ascending node: | 271.4099° |
| argument of perigee: | 73.7769° |
| revolutions per day: | 15.31711070 |
| mean anomaly at epoch: | 286.3442° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|