View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 59066U 26145.59554811 +.00000000 +00000-0 +29236-3 0 00000
2 59066 95.3916 219.5697 0146512 47.7216 313.6323 14.93342893 03
| Epoch (UTC): | 25 May 2026 14:17:35 |
| Eccentricity: | 0.0146512 |
| inclination: | 95.3916° |
| perigee height: | 485 km |
| apogee height: | 690 km |
| right ascension of ascending node: | 219.5697° |
| argument of perigee: | 47.7216° |
| revolutions per day: | 14.93342893 |
| mean anomaly at epoch: | 313.6323° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|