View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 56320U 26145.47179549 +.00000000 +00000-0 +75868-4 0 00001
2 56320 97.4466 145.3586 0002176 94.3098 265.8377 15.05652211 01
| Epoch (UTC): | 25 May 2026 11:19:23 |
| Eccentricity: | 0.0002176 |
| inclination: | 97.4466° |
| perigee height: | 548 km |
| apogee height: | 551 km |
| right ascension of ascending node: | 145.3586° |
| argument of perigee: | 94.3098° |
| revolutions per day: | 15.05652211 |
| mean anomaly at epoch: | 265.8377° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|