View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 48880U 26145.53622997 +.00000000 +00000-0 +30900-2 0 00006
2 48880 97.6612 274.5509 0001902 72.3862 287.7620 15.94920334 05
| Epoch (UTC): | 25 May 2026 12:52:10 |
| Eccentricity: | 0.0001902 |
| inclination: | 97.6612° |
| perigee height: | 287 km |
| apogee height: | 290 km |
| right ascension of ascending node: | 274.5509° |
| argument of perigee: | 72.3862° |
| revolutions per day: | 15.94920334 |
| mean anomaly at epoch: | 287.7620° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|