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 23150.49583798 .00001857 00000-0 13834-3 0 9999
2 29228 69.9347 323.7461 0007509 253.3415 106.6922 15.04791768934553
| Epoch (UTC): | 30 May 2023 11:54:00 |
| Eccentricity: | 0.0007509 |
| inclination: | 69.9347° |
| perigee height: | 547 km |
| apogee height: | 557 km |
| right ascension of ascending node: | 323.7461° |
| argument of perigee: | 253.3415° |
| revolutions per day: | 15.04791768 |
| mean anomaly at epoch: | 106.6922° |
| orbit number at epoch: | 93455 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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