View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 16263U 26017.14590133 +.00000000 +00000-0 +38998-4 0 00004
2 16263 82.5006 49.6270 0020760 90.8667 329.5054 14.85445117 08
| Epoch (UTC): | 17 January 2026 03:30:05 |
| Eccentricity: | 0.0020760 |
| inclination: | 82.5006° |
| perigee height: | 598 km |
| apogee height: | 627 km |
| right ascension of ascending node: | 49.6270° |
| argument of perigee: | 90.8667° |
| revolutions per day: | 14.85445117 |
| mean anomaly at epoch: | 329.5054° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|