View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 00058U 26149.57703800 +.00000000 +00000-0 +44802-4 0 00000
2 00058 28.3262 234.1662 0164944 53.6835 307.8819 13.46429719 02
| Epoch (UTC): | 29 May 2026 13:50:56 |
| Eccentricity: | 0.0164944 |
| inclination: | 28.3262° |
| perigee height: | 962 km |
| apogee height: | 1209 km |
| right ascension of ascending node: | 234.1662° |
| argument of perigee: | 53.6835° |
| revolutions per day: | 13.46429719 |
| mean anomaly at epoch: | 307.8819° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|