View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 17974U 26067.12241994 +.00000000 +00000-0 +32386-4 0 00000
2 17974 71.0087 36.1305 0015133 215.2407 222.1633 14.17641504 07
| Epoch (UTC): | 08 March 2026 02:56:17 |
| Eccentricity: | 0.0015133 |
| inclination: | 71.0087° |
| perigee height: | 822 km |
| apogee height: | 844 km |
| right ascension of ascending node: | 36.1305° |
| argument of perigee: | 215.2407° |
| revolutions per day: | 14.17641504 |
| mean anomaly at epoch: | 222.1633° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|