View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 58444U 26145.56164434 +.00000000 +00000-0 +36131-4 0 00007
2 58444 43.0035 327.2505 0001319 274.7404 85.3297 15.27570712 09
| Epoch (UTC): | 25 May 2026 13:28:46 |
| Eccentricity: | 0.0001319 |
| inclination: | 43.0035° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 327.2505° |
| argument of perigee: | 274.7404° |
| revolutions per day: | 15.27570712 |
| mean anomaly at epoch: | 85.3297° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|