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 42776U 17036M 24182.46059462 .06529198 23425-5 83900-3 0 9990
2 42776 97.0834 217.7889 0011559 241.2452 118.7685 16.35684810391542
| Epoch (UTC): | 30 June 2024 11:03:15 |
| Eccentricity: | 0.0011559 |
| inclination: | 97.0834° |
| perigee height: | 170 km |
| apogee height: | 185 km |
| right ascension of ascending node: | 217.7889° |
| argument of perigee: | 241.2452° |
| revolutions per day: | 16.35684810 |
| mean anomaly at epoch: | 118.7685° |
| orbit number at epoch: | 39154 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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