View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 33498U 26073.73816537 +.00000000 +00000-0 +55753-3 0 00006
2 33498 98.1468 17.2944 0010020 115.5075 244.7182 14.95001514 07
| Epoch (UTC): | 14 March 2026 17:42:57 |
| Eccentricity: | 0.0010020 |
| inclination: | 98.1468° |
| perigee height: | 575 km |
| apogee height: | 589 km |
| right ascension of ascending node: | 17.2944° |
| argument of perigee: | 115.5075° |
| revolutions per day: | 14.95001514 |
| mean anomaly at epoch: | 244.7182° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|