View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit data is extracted from the following two-line orbital elements,
1 00877U 64053B 23159.02209100 .00000253 00000-0 75624-4 0 9992
2 00877 65.0788 35.9920 0075060 321.9125 37.6681 14.59856700119914
| Epoch (UTC): | 08 June 2023 00:31:48 |
| Eccentricity: | 0.0075060 |
| inclination: | 65.0788° |
| perigee height: | 640 km |
| apogee height: | 747 km |
| right ascension of ascending node: | 35.9920° |
| argument of perigee: | 321.9125° |
| revolutions per day: | 14.59856700 |
| mean anomaly at epoch: | 37.6681° |
| orbit number at epoch: | 11991 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|