View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit data is extracted from the following two-line orbital elements,
1 33498U 09002G 25346.80861990 .00007003 00000-0 66333-3 0 9993
2 33498 98.1370 281.9782 0010166 67.5678 292.6617 14.93901404910634
| Epoch (UTC): | 12 December 2025 19:24:24 |
| Eccentricity: | 0.0010166 |
| inclination: | 98.1370° |
| perigee height: | 579 km |
| apogee height: | 593 km |
| right ascension of ascending node: | 281.9782° |
| argument of perigee: | 67.5678° |
| revolutions per day: | 14.93901404 |
| mean anomaly at epoch: | 292.6617° |
| orbit number at epoch: | 91063 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|