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 15071U 84065C 22294.72185744 0.00003999 00000-0 37135-3 0 09
2 15071 95.8843 99.4923 0005207 299.3545 60.6287 14.94467435 06
| Epoch (UTC): | 21 October 2022 17:19:28 |
| Eccentricity: | 0.0005207 |
| inclination: | 95.8843° |
| perigee height: | 580 km |
| apogee height: | 587 km |
| right ascension of ascending node: | 99.4923° |
| argument of perigee: | 299.3545° |
| revolutions per day: | 14.94467435 |
| mean anomaly at epoch: | 60.6287° |
| orbit number at epoch: | 0 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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