View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 56319U 26145.28349375 +.00000000 +00000-0 -72899-3 0 00005
2 56319 97.4512 145.3039 0001848 70.9949 289.1478 15.05707011 04
| Epoch (UTC): | 25 May 2026 06:48:13 |
| Eccentricity: | 0.0001848 |
| inclination: | 97.4512° |
| perigee height: | 548 km |
| apogee height: | 551 km |
| right ascension of ascending node: | 145.3039° |
| argument of perigee: | 70.9949° |
| revolutions per day: | 15.05707011 |
| mean anomaly at epoch: | 289.1478° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|