View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 48663U 26145.62160953 +.00000000 +00000-0 +14001-3 0 00009
2 48663 53.1603 106.0839 0001177 75.7730 284.3402 15.31702982 00
| Epoch (UTC): | 25 May 2026 14:55:07 |
| Eccentricity: | 0.0001177 |
| inclination: | 53.1603° |
| perigee height: | 470 km |
| apogee height: | 472 km |
| right ascension of ascending node: | 106.0839° |
| argument of perigee: | 75.7730° |
| revolutions per day: | 15.31702982 |
| mean anomaly at epoch: | 284.3402° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|