View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 27665U 26036.73031634 +.00000000 +00000-0 +10724-3 0 00000
2 27665 39.5740 235.4021 0010052 268.6118 186.5108 14.29512610 03
| Epoch (UTC): | 05 February 2026 17:31:39 |
| Eccentricity: | 0.0010052 |
| inclination: | 39.5740° |
| perigee height: | 786 km |
| apogee height: | 801 km |
| right ascension of ascending node: | 235.4021° |
| argument of perigee: | 268.6118° |
| revolutions per day: | 14.29512610 |
| mean anomaly at epoch: | 186.5108° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|