View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 27386U 26139.87310028 +.00000000 +00000-0 +28869-4 0 00006
2 27386 98.3821 91.8259 0001229 92.0451 288.6453 14.39057259 09
| Epoch (UTC): | 19 May 2026 20:57:15 |
| Eccentricity: | 0.0001229 |
| inclination: | 98.3821° |
| perigee height: | 761 km |
| apogee height: | 762 km |
| right ascension of ascending node: | 91.8259° |
| argument of perigee: | 92.0451° |
| revolutions per day: | 14.39057259 |
| mean anomaly at epoch: | 288.6453° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|