View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 48101U 26145.46606697 +.00000000 +00000-0 -71041-4 0 00007
2 48101 53.1593 157.9631 0001479 84.0721 276.0449 15.31687256 03
| Epoch (UTC): | 25 May 2026 11:11:08 |
| Eccentricity: | 0.0001479 |
| inclination: | 53.1593° |
| perigee height: | 470 km |
| apogee height: | 472 km |
| right ascension of ascending node: | 157.9631° |
| argument of perigee: | 84.0721° |
| revolutions per day: | 15.31687256 |
| mean anomaly at epoch: | 276.0449° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|