View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 23628U 26140.41417645 +.00000000 +00000-0 +00000-0 0 00009
2 23628 13.3956 15.8832 0003065 255.8541 13.6190 0.98662404 00
| Epoch (UTC): | 20 May 2026 09:56:24 |
| Eccentricity: | 0.0003065 |
| inclination: | 13.3956° |
| perigee height: | 36231 km |
| apogee height: | 36257 km |
| right ascension of ascending node: | 15.8832° |
| argument of perigee: | 255.8541° |
| revolutions per day: | 0.98662404 |
| mean anomaly at epoch: | 13.6190° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|