View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 48151U 26145.43776705 +.00000000 +00000-0 +48006-4 0 00001
2 48151 53.1589 155.7073 0001236 82.5399 277.5743 15.31698224 04
| Epoch (UTC): | 25 May 2026 10:30:23 |
| Eccentricity: | 0.0001236 |
| inclination: | 53.1589° |
| perigee height: | 470 km |
| apogee height: | 472 km |
| right ascension of ascending node: | 155.7073° |
| argument of perigee: | 82.5399° |
| revolutions per day: | 15.31698224 |
| mean anomaly at epoch: | 277.5743° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|