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 23657U 95046A 22147.34563931 .00001098 00000-0 12039-3 0 9993
2 23657 82.5278 4.2488 0020730 221.2440 138.7212 14.86689644445272
| Epoch (UTC): | 27 May 2022 08:17:43 |
| Eccentricity: | 0.0020730 |
| inclination: | 82.5278° |
| perigee height: | 594 km |
| apogee height: | 623 km |
| right ascension of ascending node: | 4.2488° |
| argument of perigee: | 221.2440° |
| revolutions per day: | 14.86689644 |
| mean anomaly at epoch: | 138.7212° |
| orbit number at epoch: | 44527 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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