View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 58025U 26145.62521162 +.00000000 +00000-0 +33748-3 0 00004
2 58025 97.5706 222.2323 0004030 189.3978 170.7180 15.15647011 09
| Epoch (UTC): | 25 May 2026 15:00:18 |
| Eccentricity: | 0.0004030 |
| inclination: | 97.5706° |
| perigee height: | 516 km |
| apogee height: | 522 km |
| right ascension of ascending node: | 222.2323° |
| argument of perigee: | 189.3978° |
| revolutions per day: | 15.15647011 |
| mean anomaly at epoch: | 170.7180° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|