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 35933U 09051C 23271.11116157 .00001640 00000-0 36850-3 0 9992
2 35933 98.4969 145.0657 0006931 65.8625 294.3297 14.57872510744369
| Epoch (UTC): | 28 September 2023 02:40:04 |
| Eccentricity: | 0.0006931 |
| inclination: | 98.4969° |
| perigee height: | 695 km |
| apogee height: | 705 km |
| right ascension of ascending node: | 145.0657° |
| argument of perigee: | 65.8625° |
| revolutions per day: | 14.57872510 |
| mean anomaly at epoch: | 294.3297° |
| orbit number at epoch: | 74436 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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