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 09662U 77002B 23150.76476940 .00000134 00000-0 80152-4 0 9991
2 09662 81.2731 156.9076 0053194 126.7881 233.8184 14.01035351370705
| Epoch (UTC): | 30 May 2023 18:21:16 |
| Eccentricity: | 0.0053194 |
| inclination: | 81.2731° |
| perigee height: | 851 km |
| apogee height: | 929 km |
| right ascension of ascending node: | 156.9076° |
| argument of perigee: | 126.7881° |
| revolutions per day: | 14.01035351 |
| mean anomaly at epoch: | 233.8184° |
| orbit number at epoch: | 37070 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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