View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 66372U 26145.53402666 +.00000000 +00000-0 +35786-3 0 00009
2 66372 53.1573 233.1478 0000951 92.3117 267.7993 15.30201535 04
| Epoch (UTC): | 25 May 2026 12:48:59 |
| Eccentricity: | 0.0000951 |
| inclination: | 53.1573° |
| perigee height: | 475 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 233.1478° |
| argument of perigee: | 92.3117° |
| revolutions per day: | 15.30201535 |
| mean anomaly at epoch: | 267.7993° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|