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 22915U 93074A 23270.05867751 -.00000179 00000-0 00000-0 0 9993
2 22915 12.8649 22.1296 0005728 32.0280 340.2078 0.98535123 15118
| Epoch (UTC): | 27 September 2023 01:24:29 |
| Eccentricity: | 0.0005728 |
| inclination: | 12.8649° |
| perigee height: | 36256 km |
| apogee height: | 36304 km |
| right ascension of ascending node: | 22.1296° |
| argument of perigee: | 32.0280° |
| revolutions per day: | 0.98535123 |
| mean anomaly at epoch: | 340.2078° |
| orbit number at epoch: | 1511 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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