View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 43678U 26108.61176536 +.00000000 +00000-0 +96997-4 0 00007
2 43678 98.1043 302.2933 0013736 10.7671 349.3843 15.00156051 07
| Epoch (UTC): | 18 April 2026 14:40:56 |
| Eccentricity: | 0.0013736 |
| inclination: | 98.1043° |
| perigee height: | 557 km |
| apogee height: | 576 km |
| right ascension of ascending node: | 302.2933° |
| argument of perigee: | 10.7671° |
| revolutions per day: | 15.00156051 |
| mean anomaly at epoch: | 349.3843° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|