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 23159.08571808 .00000984 00000-0 12409-3 0 9991
2 29092 97.8384 186.4668 0001543 92.1199 268.0192 14.84151600925673
| Epoch (UTC): | 08 June 2023 02:03:26 |
| Eccentricity: | 0.0001543 |
| inclination: | 97.8384° |
| perigee height: | 615 km |
| apogee height: | 617 km |
| right ascension of ascending node: | 186.4668° |
| argument of perigee: | 92.1199° |
| revolutions per day: | 14.84151600 |
| mean anomaly at epoch: | 268.0192° |
| orbit number at epoch: | 92567 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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