View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 17974U 26042.13472469 +.00000000 +00000-0 -59662-4 0 00004
2 17974 71.0070 88.8175 0016108 249.0225 141.7463 14.17638620 06
| Epoch (UTC): | 11 February 2026 03:14:00 |
| Eccentricity: | 0.0016108 |
| inclination: | 71.0070° |
| perigee height: | 822 km |
| apogee height: | 845 km |
| right ascension of ascending node: | 88.8175° |
| argument of perigee: | 249.0225° |
| revolutions per day: | 14.17638620 |
| mean anomaly at epoch: | 141.7463° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|