View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 27940U 26041.93186133 +.00000000 +00000-0 +14698-3 0 00003
2 27940 98.3776 216.5858 0013716 39.1283 321.0911 14.69322717 02
| Epoch (UTC): | 10 February 2026 22:21:52 |
| Eccentricity: | 0.0013716 |
| inclination: | 98.3776° |
| perigee height: | 654 km |
| apogee height: | 673 km |
| right ascension of ascending node: | 216.5858° |
| argument of perigee: | 39.1283° |
| revolutions per day: | 14.69322717 |
| mean anomaly at epoch: | 321.0911° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|