View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 39341U 26111.12261003 +.00000000 +00000-0 +87629-3 0 00004
2 39341 19.3283 359.8478 6677355 329.0141 4.8840 2.97681233 06
| Epoch (UTC): | 21 April 2026 02:56:33 |
| Eccentricity: | 0.6677355 |
| inclination: | 19.3283° |
| perigee height: | 404 km |
| apogee height: | 27665 km |
| right ascension of ascending node: | 359.8478° |
| argument of perigee: | 329.0141° |
| revolutions per day: | 2.97681233 |
| mean anomaly at epoch: | 4.8840° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|