View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 37741U 26145.47088110 +.00000000 +00000-0 +10227-3 0 00007
2 37741 52.0007 311.0724 0000703 114.0949 281.6629 12.62263334 00
| Epoch (UTC): | 25 May 2026 11:18:04 |
| Eccentricity: | 0.0000703 |
| inclination: | 52.0007° |
| perigee height: | 1413 km |
| apogee height: | 1414 km |
| right ascension of ascending node: | 311.0724° |
| argument of perigee: | 114.0949° |
| revolutions per day: | 12.62263334 |
| mean anomaly at epoch: | 281.6629° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|