View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 27868U 26104.18711876 +.00000000 +00000-0 -86296-4 0 00002
2 27868 82.4764 9.9811 0020876 193.1656 166.8883 12.45188464 09
| Epoch (UTC): | 14 April 2026 04:29:27 |
| Eccentricity: | 0.0020876 |
| inclination: | 82.4764° |
| perigee height: | 1468 km |
| apogee height: | 1501 km |
| right ascension of ascending node: | 9.9811° |
| argument of perigee: | 193.1656° |
| revolutions per day: | 12.45188464 |
| mean anomaly at epoch: | 166.8883° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|