View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 28089U 26145.56128490 +.00000000 +00000-0 +00000-0 0 00003
2 28089 6.2885 71.2054 0003269 332.7565 204.7982 1.00271924 06
| Epoch (UTC): | 25 May 2026 13:28:15 |
| Eccentricity: | 0.0003269 |
| inclination: | 6.2885° |
| perigee height: | 35773 km |
| apogee height: | 35800 km |
| right ascension of ascending node: | 71.2054° |
| argument of perigee: | 332.7565° |
| revolutions per day: | 1.00271924 |
| mean anomaly at epoch: | 204.7982° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|