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 23155.81365300 .00001995 00000-0 14800-3 0 9994
2 29228 69.9358 310.1593 0007396 249.2280 110.8090 15.04815949935382
| Epoch (UTC): | 04 June 2023 19:31:39 |
| Eccentricity: | 0.0007396 |
| inclination: | 69.9358° |
| perigee height: | 547 km |
| apogee height: | 557 km |
| right ascension of ascending node: | 310.1593° |
| argument of perigee: | 249.2280° |
| revolutions per day: | 15.04815949 |
| mean anomaly at epoch: | 110.8090° |
| orbit number at epoch: | 93538 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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