View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit data is extracted from the following two-line orbital elements,
1 31793U 07029B 23154.73419789 .00000250 00000-0 15529-3 0 9996
2 31793 70.9733 134.8671 0001578 266.8742 266.3181 14.14533938822628
| Epoch (UTC): | 03 June 2023 17:37:14 |
| Eccentricity: | 0.0001578 |
| inclination: | 70.9733° |
| perigee height: | 843 km |
| apogee height: | 845 km |
| right ascension of ascending node: | 134.8671° |
| argument of perigee: | 266.8742° |
| revolutions per day: | 14.14533938 |
| mean anomaly at epoch: | 266.3181° |
| orbit number at epoch: | 82262 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|