View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 58899U 26145.33085183 +.00000000 +00000-0 +43419-3 0 00005
2 58899 97.4140 355.0571 0008783 189.5957 170.5122 15.39161493 02
| Epoch (UTC): | 25 May 2026 07:56:25 |
| Eccentricity: | 0.0008783 |
| inclination: | 97.4140° |
| perigee height: | 443 km |
| apogee height: | 455 km |
| right ascension of ascending node: | 355.0571° |
| argument of perigee: | 189.5957° |
| revolutions per day: | 15.39161493 |
| mean anomaly at epoch: | 170.5122° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|