View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 40037U 26145.51460477 +.00000000 +00000-0 +84128-4 0 00006
2 40037 97.9949 95.5971 0012540 20.5946 339.5777 14.95424271 07
| Epoch (UTC): | 25 May 2026 12:21:01 |
| Eccentricity: | 0.0012540 |
| inclination: | 97.9949° |
| perigee height: | 572 km |
| apogee height: | 590 km |
| right ascension of ascending node: | 95.5971° |
| argument of perigee: | 20.5946° |
| revolutions per day: | 14.95424271 |
| mean anomaly at epoch: | 339.5777° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|