View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 47282U 26145.54912381 +.00000000 +00000-0 -16223-3 0 00005
2 47282 87.8960 355.1515 0001481 83.1120 277.0176 13.12443178 01
| Epoch (UTC): | 25 May 2026 13:10:44 |
| Eccentricity: | 0.0001481 |
| inclination: | 87.8960° |
| perigee height: | 1213 km |
| apogee height: | 1215 km |
| right ascension of ascending node: | 355.1515° |
| argument of perigee: | 83.1120° |
| revolutions per day: | 13.12443178 |
| mean anomaly at epoch: | 277.0176° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|