View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 66843U 26145.37172963 +.00000000 +00000-0 +33181-3 0 00005
2 66843 70.0002 141.0502 0003912 266.9604 93.1107 14.98337678 06
| Epoch (UTC): | 25 May 2026 08:55:17 |
| Eccentricity: | 0.0003912 |
| inclination: | 70.0002° |
| perigee height: | 569 km |
| apogee height: | 575 km |
| right ascension of ascending node: | 141.0502° |
| argument of perigee: | 266.9604° |
| revolutions per day: | 14.98337678 |
| mean anomaly at epoch: | 93.1107° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|