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 23156.59117989 .00000915 00000-0 11579-3 0 9991
2 29092 97.8387 184.0154 0001543 91.8143 268.3248 14.84145764925304
| Epoch (UTC): | 05 June 2023 14:11:17 |
| Eccentricity: | 0.0001543 |
| inclination: | 97.8387° |
| perigee height: | 615 km |
| apogee height: | 617 km |
| right ascension of ascending node: | 184.0154° |
| argument of perigee: | 91.8143° |
| revolutions per day: | 14.84145764 |
| mean anomaly at epoch: | 268.3248° |
| orbit number at epoch: | 92530 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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