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 35296U 97051PL 22333.06763312 .00004432 00000-0 99322-3 0 9999
2 35296 86.3103 92.1149 0005004 207.9472 152.1468 14.56446736549128
| Epoch (UTC): | 29 November 2022 01:37:23 |
| Eccentricity: | 0.0005004 |
| inclination: | 86.3103° |
| perigee height: | 701 km |
| apogee height: | 708 km |
| right ascension of ascending node: | 92.1149° |
| argument of perigee: | 207.9472° |
| revolutions per day: | 14.56446736 |
| mean anomaly at epoch: | 152.1468° |
| orbit number at epoch: | 54912 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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