View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 52145U 26145.04110427 +.00000000 +00000-0 +00000-0 0 00007
2 52145 62.6768 143.2766 6777840 272.8727 17.6833 2.00615925 05
| Epoch (UTC): | 25 May 2026 00:59:11 |
| Eccentricity: | 0.6777840 |
| inclination: | 62.6768° |
| perigee height: | 2179 km |
| apogee height: | 38177 km |
| right ascension of ascending node: | 143.2766° |
| argument of perigee: | 272.8727° |
| revolutions per day: | 2.00615925 |
| mean anomaly at epoch: | 17.6833° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|