View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 56142U 26145.19076131 +.00000000 +00000-0 +40145-4 0 00005
2 56142 43.0053 74.6379 0001172 269.4818 90.5900 15.27579221 04
| Epoch (UTC): | 25 May 2026 04:34:41 |
| Eccentricity: | 0.0001172 |
| inclination: | 43.0053° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 74.6379° |
| argument of perigee: | 269.4818° |
| revolutions per day: | 15.27579221 |
| mean anomaly at epoch: | 90.5900° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|