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 29092U 06015A 23275.64450625 .00001532 00000-0 18841-3 0 9991
2 29092 97.8324 300.9928 0001502 89.7382 270.4005 14.84424359942965
| Epoch (UTC): | 02 October 2023 15:28:05 |
| Eccentricity: | 0.0001502 |
| inclination: | 97.8324° |
| perigee height: | 614 km |
| apogee height: | 616 km |
| right ascension of ascending node: | 300.9928° |
| argument of perigee: | 89.7382° |
| revolutions per day: | 14.84424359 |
| mean anomaly at epoch: | 270.4005° |
| orbit number at epoch: | 94296 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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