View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 47978U 26145.50998183 +.00000000 +00000-0 -93954-4 0 00004
2 47978 53.1614 335.0920 0001298 77.8683 282.2464 15.31708664 07
| Epoch (UTC): | 25 May 2026 12:14:22 |
| Eccentricity: | 0.0001298 |
| inclination: | 53.1614° |
| perigee height: | 470 km |
| apogee height: | 472 km |
| right ascension of ascending node: | 335.0920° |
| argument of perigee: | 77.8683° |
| revolutions per day: | 15.31708664 |
| mean anomaly at epoch: | 282.2464° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|