View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 45138U 26145.21349780 +.00000000 +00000-0 -44765-3 0 00006
2 45138 87.8870 40.8180 0001778 95.9599 264.1730 13.10378248 01
| Epoch (UTC): | 25 May 2026 05:07:26 |
| Eccentricity: | 0.0001778 |
| inclination: | 87.8870° |
| perigee height: | 1220 km |
| apogee height: | 1223 km |
| right ascension of ascending node: | 40.8180° |
| argument of perigee: | 95.9599° |
| revolutions per day: | 13.10378248 |
| mean anomaly at epoch: | 264.1730° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|