View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 16263U 26072.32490289 +.00000000 +00000-0 +68984-4 0 00004
2 16263 82.5065 357.6464 0017565 268.4947 212.8099 14.85523525 06
| Epoch (UTC): | 13 March 2026 07:47:51 |
| Eccentricity: | 0.0017565 |
| inclination: | 82.5065° |
| perigee height: | 600 km |
| apogee height: | 624 km |
| right ascension of ascending node: | 357.6464° |
| argument of perigee: | 268.4947° |
| revolutions per day: | 14.85523525 |
| mean anomaly at epoch: | 212.8099° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|