View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 33498U 26137.31008501 +.00000000 +00000-0 +21276-3 0 00008
2 33498 98.1536 83.3678 0006947 273.0012 87.0413 14.95515891 08
| Epoch (UTC): | 17 May 2026 07:26:31 |
| Eccentricity: | 0.0006947 |
| inclination: | 98.1536° |
| perigee height: | 576 km |
| apogee height: | 586 km |
| right ascension of ascending node: | 83.3678° |
| argument of perigee: | 273.0012° |
| revolutions per day: | 14.95515891 |
| mean anomaly at epoch: | 87.0413° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|