View from above orbital plane
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View from above satellite
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Ground track
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The orbit data is extracted from the following two-line orbital elements,
1 05707U 71114B 23159.08144871 .00000283 00000-0 99248-4 0 9995
2 05707 74.0285 19.7439 0025491 274.0393 85.7848 14.39297429696404
| Epoch (UTC): | 08 June 2023 01:57:17 |
| Eccentricity: | 0.0025491 |
| inclination: | 74.0285° |
| perigee height: | 742 km |
| apogee height: | 779 km |
| right ascension of ascending node: | 19.7439° |
| argument of perigee: | 274.0393° |
| revolutions per day: | 14.39297429 |
| mean anomaly at epoch: | 85.7848° |
| orbit number at epoch: | 69640 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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