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 28415U 04035C 23150.88366836 .00002694 00000-0 16206-3 0 9990
2 28415 97.4699 188.4029 0045498 267.4668 92.1352 15.10849152 26003
| Epoch (UTC): | 30 May 2023 21:12:28 |
| Eccentricity: | 0.0045498 |
| inclination: | 97.4699° |
| perigee height: | 502 km |
| apogee height: | 565 km |
| right ascension of ascending node: | 188.4029° |
| argument of perigee: | 267.4668° |
| revolutions per day: | 15.10849152 |
| mean anomaly at epoch: | 92.1352° |
| orbit number at epoch: | 2600 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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