View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 66844U 26145.38842419 +.00000000 +00000-0 +34614-3 0 00009
2 66844 70.0006 141.1110 0003836 269.1419 90.9301 14.98334962 05
| Epoch (UTC): | 25 May 2026 09:19:19 |
| Eccentricity: | 0.0003836 |
| inclination: | 70.0006° |
| perigee height: | 569 km |
| apogee height: | 575 km |
| right ascension of ascending node: | 141.1110° |
| argument of perigee: | 269.1419° |
| revolutions per day: | 14.98334962 |
| mean anomaly at epoch: | 90.9301° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|