View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 43758U 26145.18024881 +.00000000 +00000-0 +73473-3 0 00007
2 43758 97.4544 220.8193 0006319 357.4373 2.6842 15.45179555 07
| Epoch (UTC): | 25 May 2026 04:19:33 |
| Eccentricity: | 0.0006319 |
| inclination: | 97.4544° |
| perigee height: | 427 km |
| apogee height: | 435 km |
| right ascension of ascending node: | 220.8193° |
| argument of perigee: | 357.4373° |
| revolutions per day: | 15.45179555 |
| mean anomaly at epoch: | 2.6842° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|