View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 38042U 26145.15603962 +.00000000 +00000-0 +15101-4 0 00002
2 38042 52.0094 44.6042 0000393 75.3454 89.3088 12.62269415 06
| Epoch (UTC): | 25 May 2026 03:44:41 |
| Eccentricity: | 0.0000393 |
| inclination: | 52.0094° |
| perigee height: | 1413 km |
| apogee height: | 1414 km |
| right ascension of ascending node: | 44.6042° |
| argument of perigee: | 75.3454° |
| revolutions per day: | 12.62269415 |
| mean anomaly at epoch: | 89.3088° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|