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 23154.65874126 .00003904 00000-0 23279-3 0 9998
2 28415 97.4691 192.0894 0045671 254.0340 105.5856 15.10876015 26576
| Epoch (UTC): | 03 June 2023 15:48:35 |
| Eccentricity: | 0.0045671 |
| inclination: | 97.4691° |
| perigee height: | 502 km |
| apogee height: | 565 km |
| right ascension of ascending node: | 192.0894° |
| argument of perigee: | 254.0340° |
| revolutions per day: | 15.10876015 |
| mean anomaly at epoch: | 105.5856° |
| orbit number at epoch: | 2657 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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