View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 16719U 26040.62975766 +.00000000 +00000-0 +44599-3 0 00001
2 16719 82.5330 103.2323 0005023 49.4090 310.7601 15.56514050 07
| Epoch (UTC): | 09 February 2026 15:06:51 |
| Eccentricity: | 0.0005023 |
| inclination: | 82.5330° |
| perigee height: | 394 km |
| apogee height: | 401 km |
| right ascension of ascending node: | 103.2323° |
| argument of perigee: | 49.4090° |
| revolutions per day: | 15.56514050 |
| mean anomaly at epoch: | 310.7601° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|