View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 58490U 26145.29999648 +.00000000 +00000-0 +43816-4 0 00009
2 58490 43.0063 350.9213 0001981 282.8406 77.2224 15.27586323 02
| Epoch (UTC): | 25 May 2026 07:11:59 |
| Eccentricity: | 0.0001981 |
| inclination: | 43.0063° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 350.9213° |
| argument of perigee: | 282.8406° |
| revolutions per day: | 15.27586323 |
| mean anomaly at epoch: | 77.2224° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|