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 5707U 71114B 23154.77205152 .00000285 00000-0 10006-3 0 9992
2 5707 74.0289 27.7019 0025433 282.6340 77.1971 14.39294704696005
| Epoch (UTC): | 03 June 2023 18:31:45 |
| Eccentricity: | 0.0025433 |
| inclination: | 74.0289° |
| perigee height: | 742 km |
| apogee height: | 779 km |
| right ascension of ascending node: | 27.7019° |
| argument of perigee: | 282.6340° |
| revolutions per day: | 14.39294704 |
| mean anomaly at epoch: | 77.1971° |
| orbit number at epoch: | 69600 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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