View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 40017U 26053.83614038 +.00000000 +00000-0 +51085-3 0 00006
2 40017 98.0361 121.2615 0010788 243.2806 116.7322 15.15903041 09
| Epoch (UTC): | 22 February 2026 20:04:02 |
| Eccentricity: | 0.0010788 |
| inclination: | 98.0361° |
| perigee height: | 511 km |
| apogee height: | 526 km |
| right ascension of ascending node: | 121.2615° |
| argument of perigee: | 243.2806° |
| revolutions per day: | 15.15903041 |
| mean anomaly at epoch: | 116.7322° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|