View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 47399U 26145.13381118 +.00000000 +00000-0 +19290-3 0 00003
2 47399 53.1586 41.1567 0001107 91.0907 269.0221 15.31719828 08
| Epoch (UTC): | 25 May 2026 03:12:41 |
| Eccentricity: | 0.0001107 |
| inclination: | 53.1586° |
| perigee height: | 470 km |
| apogee height: | 471 km |
| right ascension of ascending node: | 41.1567° |
| argument of perigee: | 91.0907° |
| revolutions per day: | 15.31719828 |
| mean anomaly at epoch: | 269.0221° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|