View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 10121U 26046.18010500 +.00000000 +00000-0 +90283-4 0 00007
2 10121 74.0442 83.0402 0018204 8.6657 351.4807 14.37342161 02
| Epoch (UTC): | 15 February 2026 04:19:21 |
| Eccentricity: | 0.0018204 |
| inclination: | 74.0442° |
| perigee height: | 754 km |
| apogee height: | 780 km |
| right ascension of ascending node: | 83.0402° |
| argument of perigee: | 8.6657° |
| revolutions per day: | 14.37342161 |
| mean anomaly at epoch: | 351.4807° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|