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 23154.56857426 .00000923 00000-0 11682-3 0 9997
2 29092 97.8388 182.0277 0001552 92.0185 268.1207 14.84141848925007
| Epoch (UTC): | 03 June 2023 13:38:44 |
| Eccentricity: | 0.0001552 |
| inclination: | 97.8388° |
| perigee height: | 615 km |
| apogee height: | 617 km |
| right ascension of ascending node: | 182.0277° |
| argument of perigee: | 92.0185° |
| revolutions per day: | 14.84141848 |
| mean anomaly at epoch: | 268.1207° |
| orbit number at epoch: | 92500 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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