View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 43432U 26145.39523065 +.00000000 +00000-0 +00000-0 0 00000
2 43432 0.0147 3.0496 0000471 211.5213 298.7509 1.00272795 02
| Epoch (UTC): | 25 May 2026 09:29:07 |
| Eccentricity: | 0.0000471 |
| inclination: | 0.0147° |
| perigee height: | 35784 km |
| apogee height: | 35788 km |
| right ascension of ascending node: | 3.0496° |
| argument of perigee: | 211.5213° |
| revolutions per day: | 1.00272795 |
| mean anomaly at epoch: | 298.7509° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|