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 23151.89177300 .00002110 00000-0 15613-3 0 9992
2 29228 69.9359 320.1799 0007527 252.4097 107.6243 15.04798550934796
| Epoch (UTC): | 31 May 2023 21:24:09 |
| Eccentricity: | 0.0007527 |
| inclination: | 69.9359° |
| perigee height: | 547 km |
| apogee height: | 557 km |
| right ascension of ascending node: | 320.1799° |
| argument of perigee: | 252.4097° |
| revolutions per day: | 15.04798550 |
| mean anomaly at epoch: | 107.6243° |
| orbit number at epoch: | 93479 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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