View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 47796U 26145.63832852 +.00000000 +00000-0 +11870-2 0 00000
2 47796 53.1577 241.1004 0001440 24.1248 335.9820 15.32456174 03
| Epoch (UTC): | 25 May 2026 15:19:11 |
| Eccentricity: | 0.0001440 |
| inclination: | 53.1577° |
| perigee height: | 468 km |
| apogee height: | 469 km |
| right ascension of ascending node: | 241.1004° |
| argument of perigee: | 24.1248° |
| revolutions per day: | 15.32456174 |
| mean anomaly at epoch: | 335.9820° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|