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 29228U 06021A 23156.81073399 .00002224 00000-0 16411-3 0 9995
2 29228 69.9360 307.6117 0007378 248.1869 111.8509 15.04820895935505
| Epoch (UTC): | 05 June 2023 19:27:27 |
| Eccentricity: | 0.0007378 |
| inclination: | 69.9360° |
| perigee height: | 547 km |
| apogee height: | 557 km |
| right ascension of ascending node: | 307.6117° |
| argument of perigee: | 248.1869° |
| revolutions per day: | 15.04820895 |
| mean anomaly at epoch: | 111.8509° |
| orbit number at epoch: | 93550 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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