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 23151.87711404 .00002904 00000-0 17430-3 0 9999
2 28415 97.4697 189.3730 0045516 263.9034 95.7008 15.10855728 26158
| Epoch (UTC): | 31 May 2023 21:03:02 |
| Eccentricity: | 0.0045516 |
| inclination: | 97.4697° |
| perigee height: | 502 km |
| apogee height: | 565 km |
| right ascension of ascending node: | 189.3730° |
| argument of perigee: | 263.9034° |
| revolutions per day: | 15.10855728 |
| mean anomaly at epoch: | 95.7008° |
| orbit number at epoch: | 2615 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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