View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 28184U 26145.45309352 +.00000000 +00000-0 +00000-0 0 00005
2 28184 5.9852 72.2783 0005353 352.4337 42.4558 1.00274214 05
| Epoch (UTC): | 25 May 2026 10:52:27 |
| Eccentricity: | 0.0005353 |
| inclination: | 5.9852° |
| perigee height: | 35763 km |
| apogee height: | 35808 km |
| right ascension of ascending node: | 72.2783° |
| argument of perigee: | 352.4337° |
| revolutions per day: | 1.00274214 |
| mean anomaly at epoch: | 42.4558° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|