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 22230.08852561 .00001821 00000-0 11814-3 0 9996
2 28415 97.5121 269.2037 0050266 166.9125 193.3421 15.08313334982884
| Epoch (UTC): | 18 August 2022 02:07:28 |
| Eccentricity: | 0.0050266 |
| inclination: | 97.5121° |
| perigee height: | 506 km |
| apogee height: | 576 km |
| right ascension of ascending node: | 269.2037° |
| argument of perigee: | 166.9125° |
| revolutions per day: | 15.08313334 |
| mean anomaly at epoch: | 193.3421° |
| orbit number at epoch: | 98288 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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