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 23078.76306356 -.00000192 00000-0 00000+0 0 9990
2 22915 12.6923 23.3593 0009344 10.2632 182.8002 0.98534294 13204
| Epoch (UTC): | 19 March 2023 18:18:48 |
| Eccentricity: | 0.0009344 |
| inclination: | 12.6923° |
| perigee height: | 36240 km |
| apogee height: | 36320 km |
| right ascension of ascending node: | 23.3593° |
| argument of perigee: | 10.2632° |
| revolutions per day: | 0.98534294 |
| mean anomaly at epoch: | 182.8002° |
| orbit number at epoch: | 1320 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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