View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 47274U 26145.31192647 +.00000000 +00000-0 -70341-3 0 00007
2 47274 87.8947 355.2345 0001720 76.1102 284.0218 13.12442265 08
| Epoch (UTC): | 25 May 2026 07:29:10 |
| Eccentricity: | 0.0001720 |
| inclination: | 87.8947° |
| perigee height: | 1212 km |
| apogee height: | 1215 km |
| right ascension of ascending node: | 355.2345° |
| argument of perigee: | 76.1102° |
| revolutions per day: | 13.12442265 |
| mean anomaly at epoch: | 284.0218° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|