View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 27939U 26110.98109166 +.00000000 +00000-0 +20949-3 0 00000
2 27939 98.3462 293.7279 0012600 89.9532 62.7309 14.73363257 06
| Epoch (UTC): | 20 April 2026 23:32:46 |
| Eccentricity: | 0.0012600 |
| inclination: | 98.3462° |
| perigee height: | 641 km |
| apogee height: | 659 km |
| right ascension of ascending node: | 293.7279° |
| argument of perigee: | 89.9532° |
| revolutions per day: | 14.73363257 |
| mean anomaly at epoch: | 62.7309° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|