View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 47275U 26145.29160021 +.00000000 +00000-0 -79464-3 0 00001
2 47275 87.8959 355.2100 0001211 125.0890 235.0352 13.12440850 07
| Epoch (UTC): | 25 May 2026 06:59:54 |
| Eccentricity: | 0.0001211 |
| inclination: | 87.8959° |
| perigee height: | 1213 km |
| apogee height: | 1215 km |
| right ascension of ascending node: | 355.2100° |
| argument of perigee: | 125.0890° |
| revolutions per day: | 13.12440850 |
| mean anomaly at epoch: | 235.0352° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|