View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 49308U 26145.34267516 +.00000000 +00000-0 +11987-3 0 00008
2 49308 87.9175 278.9894 0002187 95.3029 264.8354 13.20771921 01
| Epoch (UTC): | 25 May 2026 08:13:27 |
| Eccentricity: | 0.0002187 |
| inclination: | 87.9175° |
| perigee height: | 1180 km |
| apogee height: | 1183 km |
| right ascension of ascending node: | 278.9894° |
| argument of perigee: | 95.3029° |
| revolutions per day: | 13.20771921 |
| mean anomaly at epoch: | 264.8354° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|