View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 29517U 26153.36951994 +.00000000 +00000-0 +99569-4 0 00002
2 29517 28.2443 111.5814 4044428 269.7090 45.2120 6.89907476 09
| Epoch (UTC): | 02 June 2026 08:52:06 |
| Eccentricity: | 0.4044428 |
| inclination: | 28.2443° |
| perigee height: | 564 km |
| apogee height: | 9992 km |
| right ascension of ascending node: | 111.5814° |
| argument of perigee: | 269.7090° |
| revolutions per day: | 6.89907476 |
| mean anomaly at epoch: | 45.2120° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|