View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit data is extracted from the following two-line orbital elements,
1 00085U 61004C 23332.53882740 .00037091 00000-0 56613-2 0 9997
2 00085 38.7520 10.1407 0291319 340.0967 18.8617 14.48436558111043
Epoch (UTC): | 28 November 2023 12:55:54 |
Eccentricity: | 0.0291319 |
inclination: | 38.7520° |
perigee height: | 523 km |
apogee height: | 938 km |
right ascension of ascending node: | 10.1407° |
argument of perigee: | 340.0967° |
revolutions per day: | 14.48436558 |
mean anomaly at epoch: | 18.8617° |
orbit number at epoch: | 11104 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|