View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 56331U 26145.46902506 +.00000000 +00000-0 +22209-4 0 00000
2 56331 97.4479 145.3651 0001691 111.5562 248.5846 15.05652838 03
| Epoch (UTC): | 25 May 2026 11:15:23 |
| Eccentricity: | 0.0001691 |
| inclination: | 97.4479° |
| perigee height: | 548 km |
| apogee height: | 551 km |
| right ascension of ascending node: | 145.3651° |
| argument of perigee: | 111.5562° |
| revolutions per day: | 15.05652838 |
| mean anomaly at epoch: | 248.5846° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|