View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 43804U 26111.41940142 +.00000000 +00000-0 +40999-3 0 00002
2 43804 97.4231 172.0677 0011817 119.1622 241.0801 15.27111368 08
| Epoch (UTC): | 21 April 2026 10:03:56 |
| Eccentricity: | 0.0011817 |
| inclination: | 97.4231° |
| perigee height: | 476 km |
| apogee height: | 493 km |
| right ascension of ascending node: | 172.0677° |
| argument of perigee: | 119.1622° |
| revolutions per day: | 15.27111368 |
| mean anomaly at epoch: | 241.0801° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|