View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 16494U 26100.32275762 +.00000000 +00000-0 +51585-4 0 00008
2 16494 82.9353 197.0787 0018488 232.3618 191.9409 13.76780087 09
| Epoch (UTC): | 10 April 2026 07:44:46 |
| Eccentricity: | 0.0018488 |
| inclination: | 82.9353° |
| perigee height: | 962 km |
| apogee height: | 989 km |
| right ascension of ascending node: | 197.0787° |
| argument of perigee: | 232.3618° |
| revolutions per day: | 13.76780087 |
| mean anomaly at epoch: | 191.9409° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|