View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 43683U 26145.66178933 +.00000000 +00000-0 +00000-0 0 00008
2 43683 2.8135 97.9833 0008053 342.4972 200.9762 1.00271534 00
| Epoch (UTC): | 25 May 2026 15:52:58 |
| Eccentricity: | 0.0008053 |
| inclination: | 2.8135° |
| perigee height: | 35753 km |
| apogee height: | 35821 km |
| right ascension of ascending node: | 97.9833° |
| argument of perigee: | 342.4972° |
| revolutions per day: | 1.00271534 |
| mean anomaly at epoch: | 200.9762° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|