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 1392U 65020AH 24286.12958942 .00037624 00000-0 32510-2 0 9995
2 1392 55.8701 240.0632 0244872 196.3072 162.9960 14.76636270 3889
| Epoch (UTC): | 12 October 2024 03:06:36 |
| Eccentricity: | 0.0244872 |
| inclination: | 55.8701° |
| perigee height: | 468 km |
| apogee height: | 812 km |
| right ascension of ascending node: | 240.0632° |
| argument of perigee: | 196.3072° |
| revolutions per day: | 14.76636270 |
| mean anomaly at epoch: | 162.9960° |
| orbit number at epoch: | 388 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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