View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 47851U 26144.75727019 +.00000000 +00000-0 +00000-0 0 00003
2 47851 16.5785 302.7493 0014494 25.6909 333.1870 1.00278141 09
| Epoch (UTC): | 24 May 2026 18:10:28 |
| Eccentricity: | 0.0014494 |
| inclination: | 16.5785° |
| perigee height: | 35724 km |
| apogee height: | 35846 km |
| right ascension of ascending node: | 302.7493° |
| argument of perigee: | 25.6909° |
| revolutions per day: | 1.00278141 |
| mean anomaly at epoch: | 333.1870° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|