View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 00053U 26135.23584251 +.00000000 +00000-0 +90318-3 0 00002
2 00053 47.2772 83.9768 0101092 338.0515 21.5962 12.17412372 03
| Epoch (UTC): | 15 May 2026 05:39:36 |
| Eccentricity: | 0.0101092 |
| inclination: | 47.2772° |
| perigee height: | 1523 km |
| apogee height: | 1685 km |
| right ascension of ascending node: | 83.9768° |
| argument of perigee: | 338.0515° |
| revolutions per day: | 12.17412372 |
| mean anomaly at epoch: | 21.5962° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|