View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 58129U 26145.16828032 +.00000000 +00000-0 +62356-5 0 00003
2 58129 43.0035 60.5560 0001445 265.9116 94.1570 15.27568656 05
| Epoch (UTC): | 25 May 2026 04:02:19 |
| Eccentricity: | 0.0001445 |
| inclination: | 43.0035° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 60.5560° |
| argument of perigee: | 265.9116° |
| revolutions per day: | 15.27568656 |
| mean anomaly at epoch: | 94.1570° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|