View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 66132U 26145.12159067 +.00000000 +00000-0 +50054-3 0 00007
2 66132 53.1600 44.5270 0001247 59.8026 300.3098 15.30199989 08
| Epoch (UTC): | 25 May 2026 02:55:05 |
| Eccentricity: | 0.0001247 |
| inclination: | 53.1600° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 44.5270° |
| argument of perigee: | 59.8026° |
| revolutions per day: | 15.30199989 |
| mean anomaly at epoch: | 300.3098° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|