View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 28230U 26150.21951263 +.00000000 +00000-0 +11397-3 0 00005
2 28230 89.8522 50.5346 0002683 73.2182 286.9338 14.83255669 04
| Epoch (UTC): | 30 May 2026 05:16:05 |
| Eccentricity: | 0.0002683 |
| inclination: | 89.8522° |
| perigee height: | 617 km |
| apogee height: | 621 km |
| right ascension of ascending node: | 50.5346° |
| argument of perigee: | 73.2182° |
| revolutions per day: | 14.83255669 |
| mean anomaly at epoch: | 286.9338° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|