View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 27844U 26133.96662765 +.00000000 +00000-0 +10178-3 0 00000
2 27844 98.6747 142.9554 0008324 287.2736 72.7532 14.24313628 00
| Epoch (UTC): | 13 May 2026 23:11:56 |
| Eccentricity: | 0.0008324 |
| inclination: | 98.6747° |
| perigee height: | 805 km |
| apogee height: | 817 km |
| right ascension of ascending node: | 142.9554° |
| argument of perigee: | 287.2736° |
| revolutions per day: | 14.24313628 |
| mean anomaly at epoch: | 72.7532° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|