View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 52787U 26145.56761189 +.00000000 +00000-0 +22854-3 0 00007
2 52787 49.9881 305.8593 0007999 19.1374 340.9862 14.81288498 07
| Epoch (UTC): | 25 May 2026 13:37:21 |
| Eccentricity: | 0.0007999 |
| inclination: | 49.9881° |
| perigee height: | 620 km |
| apogee height: | 631 km |
| right ascension of ascending node: | 305.8593° |
| argument of perigee: | 19.1374° |
| revolutions per day: | 14.81288498 |
| mean anomaly at epoch: | 340.9862° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|