View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 66124U 26144.99306919 +.00000000 +00000-0 +33360-3 0 00003
2 66124 53.1602 45.1448 0001223 93.2267 266.8874 15.30212549 04
| Epoch (UTC): | 24 May 2026 23:50:01 |
| Eccentricity: | 0.0001223 |
| inclination: | 53.1602° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 45.1448° |
| argument of perigee: | 93.2267° |
| revolutions per day: | 15.30212549 |
| mean anomaly at epoch: | 266.8874° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|