View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 19419U 26106.28743830 +.00000000 +00000-0 +92282-4 0 00004
2 19419 90.0454 20.7038 0094111 250.8088 226.4178 13.42648972 01
| Epoch (UTC): | 16 April 2026 06:53:54 |
| Eccentricity: | 0.0094111 |
| inclination: | 90.0454° |
| perigee height: | 1029 km |
| apogee height: | 1170 km |
| right ascension of ascending node: | 20.7038° |
| argument of perigee: | 250.8088° |
| revolutions per day: | 13.42648972 |
| mean anomaly at epoch: | 226.4178° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|