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 23161.10831059 .00001009 00000-0 12707-3 0 9994
2 29092 97.8383 188.4545 0001523 92.2887 267.8502 14.84155815926070
| Epoch (UTC): | 10 June 2023 02:35:58 |
| Eccentricity: | 0.0001523 |
| inclination: | 97.8383° |
| perigee height: | 615 km |
| apogee height: | 617 km |
| right ascension of ascending node: | 188.4545° |
| argument of perigee: | 92.2887° |
| revolutions per day: | 14.84155815 |
| mean anomaly at epoch: | 267.8502° |
| orbit number at epoch: | 92607 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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