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 57764U 23133H 24251.76882134 .00000197 00000-0 16313-3 0 9998
2 57764 80.9958 268.7777 0005536 316.9874 43.0849 13.85529899 51396
| Epoch (UTC): | 07 September 2024 18:27:06 |
| Eccentricity: | 0.0005536 |
| inclination: | 80.9958° |
| perigee height: | 940 km |
| apogee height: | 948 km |
| right ascension of ascending node: | 268.7777° |
| argument of perigee: | 316.9874° |
| revolutions per day: | 13.85529899 |
| mean anomaly at epoch: | 43.0849° |
| orbit number at epoch: | 5139 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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