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 23333.29065930 .00006522 00000-0 80101-3 0 9994
2 33498 98.1253 238.8259 0009895 349.0792 11.0205 14.83374303800293
| Epoch (UTC): | 29 November 2023 06:58:32 |
| Eccentricity: | 0.0009895 |
| inclination: | 98.1253° |
| perigee height: | 612 km |
| apogee height: | 625 km |
| right ascension of ascending node: | 238.8259° |
| argument of perigee: | 349.0792° |
| revolutions per day: | 14.83374303 |
| mean anomaly at epoch: | 11.0205° |
| orbit number at epoch: | 80029 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|