View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 27046U 26107.26850958 +.00000000 +00000-0 -17803-2 0 00003
2 27046 8.2827 14.2047 7090935 214.4394 335.7093 2.24255897 00
| Epoch (UTC): | 17 April 2026 06:26:39 |
| Eccentricity: | 0.7090935 |
| inclination: | 8.2827° |
| perigee height: | 794 km |
| apogee height: | 35760 km |
| right ascension of ascending node: | 14.2047° |
| argument of perigee: | 214.4394° |
| revolutions per day: | 2.24255897 |
| mean anomaly at epoch: | 335.7093° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|