View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 55757U 26145.14311093 +.00000000 +00000-0 -19971-4 0 00004
2 55757 70.0003 51.6332 0002647 270.0762 90.0094 14.98334258 03
| Epoch (UTC): | 25 May 2026 03:26:04 |
| Eccentricity: | 0.0002647 |
| inclination: | 70.0003° |
| perigee height: | 570 km |
| apogee height: | 574 km |
| right ascension of ascending node: | 51.6332° |
| argument of perigee: | 270.0762° |
| revolutions per day: | 14.98334258 |
| mean anomaly at epoch: | 90.0094° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|