View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 48047U 26145.47817265 +.00000000 +00000-0 +74769-3 0 00000
2 48047 87.8948 324.7375 0001962 95.4398 264.6955 13.13468986 02
| Epoch (UTC): | 25 May 2026 11:28:34 |
| Eccentricity: | 0.0001962 |
| inclination: | 87.8948° |
| perigee height: | 1208 km |
| apogee height: | 1211 km |
| right ascension of ascending node: | 324.7375° |
| argument of perigee: | 95.4398° |
| revolutions per day: | 13.13468986 |
| mean anomaly at epoch: | 264.6955° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|