View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit data is extracted from the following two-line orbital elements,
1 39090U 13009E 25080.44956038 .00001256 00000-0 44034-3 0 9990
2 39090 98.3822 267.2487 0009521 139.2308 220.9592 14.36708467632044
| Epoch (UTC): | 21 March 2025 10:47:22 |
| Eccentricity: | 0.0009521 |
| inclination: | 98.3822° |
| perigee height: | 762 km |
| apogee height: | 776 km |
| right ascension of ascending node: | 267.2487° |
| argument of perigee: | 139.2308° |
| revolutions per day: | 14.36708467 |
| mean anomaly at epoch: | 220.9592° |
| orbit number at epoch: | 63204 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|