View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 43773U 26111.83522801 +.00000000 +00000-0 +19363-3 0 00002
2 43773 97.4020 156.0682 0010703 173.1169 187.0211 15.12889946 08
| Epoch (UTC): | 21 April 2026 20:02:43 |
| Eccentricity: | 0.0010703 |
| inclination: | 97.4020° |
| perigee height: | 520 km |
| apogee height: | 535 km |
| right ascension of ascending node: | 156.0682° |
| argument of perigee: | 173.1169° |
| revolutions per day: | 15.12889946 |
| mean anomaly at epoch: | 187.0211° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|