View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 48117U 26145.44673286 +.00000000 +00000-0 +19593-4 0 00003
2 48117 53.1603 155.4862 0001118 86.2595 273.8534 15.31708166 08
| Epoch (UTC): | 25 May 2026 10:43:17 |
| Eccentricity: | 0.0001118 |
| inclination: | 53.1603° |
| perigee height: | 470 km |
| apogee height: | 471 km |
| right ascension of ascending node: | 155.4862° |
| argument of perigee: | 86.2595° |
| revolutions per day: | 15.31708166 |
| mean anomaly at epoch: | 273.8534° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|