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 25682U 99020A 23151.14430014 .00000402 00000-0 92648-4 0 9991
2 25682 97.9300 190.2078 0001820 96.0127 331.8953 14.60100780283299
| Epoch (UTC): | 31 May 2023 03:27:47 |
| Eccentricity: | 0.0001820 |
| inclination: | 97.9300° |
| perigee height: | 691 km |
| apogee height: | 694 km |
| right ascension of ascending node: | 190.2078° |
| argument of perigee: | 96.0127° |
| revolutions per day: | 14.60100780 |
| mean anomaly at epoch: | 331.8953° |
| orbit number at epoch: | 28329 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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