View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 16116U 26146.19459203 +.00000000 +00000-0 +00000-0 0 00000
2 16116 14.3802 347.6064 0001104 231.6598 298.8253 0.99326684 09
| Epoch (UTC): | 26 May 2026 04:40:12 |
| Eccentricity: | 0.0001104 |
| inclination: | 14.3802° |
| perigee height: | 36049 km |
| apogee height: | 36058 km |
| right ascension of ascending node: | 347.6064° |
| argument of perigee: | 231.6598° |
| revolutions per day: | 0.99326684 |
| mean anomaly at epoch: | 298.8253° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|