View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 48423U 26145.50687580 +.00000000 +00000-0 +13597-3 0 00009
2 48423 34.9957 169.8482 0004535 218.4026 141.6360 15.02527066 03
| Epoch (UTC): | 25 May 2026 12:09:54 |
| Eccentricity: | 0.0004535 |
| inclination: | 34.9957° |
| perigee height: | 556 km |
| apogee height: | 562 km |
| right ascension of ascending node: | 169.8482° |
| argument of perigee: | 218.4026° |
| revolutions per day: | 15.02527066 |
| mean anomaly at epoch: | 141.6360° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|