View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 49072U 26145.43542823 +.00000000 +00000-0 +79712-4 0 00004
2 49072 97.4808 148.9585 0001933 96.7382 263.4071 15.16736664 09
| Epoch (UTC): | 25 May 2026 10:27:00 |
| Eccentricity: | 0.0001933 |
| inclination: | 97.4808° |
| perigee height: | 514 km |
| apogee height: | 517 km |
| right ascension of ascending node: | 148.9585° |
| argument of perigee: | 96.7382° |
| revolutions per day: | 15.16736664 |
| mean anomaly at epoch: | 263.4071° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|