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 15378U 84112A 22140.47582119 -.00000059 00000-0 26409-4 0 9996
2 15378 64.9922 315.2164 0030400 137.3493 222.9935 13.83581295899000
| Epoch (UTC): | 20 May 2022 11:25:10 |
| Eccentricity: | 0.0030400 |
| inclination: | 64.9922° |
| perigee height: | 929 km |
| apogee height: | 973 km |
| right ascension of ascending node: | 315.2164° |
| argument of perigee: | 137.3493° |
| revolutions per day: | 13.83581295 |
| mean anomaly at epoch: | 222.9935° |
| orbit number at epoch: | 89900 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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