View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 45362U 26014.45524971 +.00000000 +00000-0 +19010-3 0 00007
2 45362 53.0212 332.8947 0005276 207.1556 152.9218 16.48330869 03
| Epoch (UTC): | 14 January 2026 10:55:33 |
| Eccentricity: | 0.0005276 |
| inclination: | 53.0212° |
| perigee height: | 140 km |
| apogee height: | 147 km |
| right ascension of ascending node: | 332.8947° |
| argument of perigee: | 207.1556° |
| revolutions per day: | 16.48330869 |
| mean anomaly at epoch: | 152.9218° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|