View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 42740U 26145.35605713 +.00000000 +00000-0 +00000-0 0 00008
2 42740 0.0136 288.9839 0000131 143.3677 228.8910 1.00271032 08
| Epoch (UTC): | 25 May 2026 08:32:43 |
| Eccentricity: | 0.0000131 |
| inclination: | 0.0136° |
| perigee height: | 35786 km |
| apogee height: | 35787 km |
| right ascension of ascending node: | 288.9839° |
| argument of perigee: | 143.3677° |
| revolutions per day: | 1.00271032 |
| mean anomaly at epoch: | 228.8910° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|