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 11870U 80056B 23151.52182209 .00000150 00000-0 59104-4 0 9996
2 11870 74.0514 173.7959 0017431 303.3495 56.5989 14.37331191223275
| Epoch (UTC): | 31 May 2023 12:31:25 |
| Eccentricity: | 0.0017431 |
| inclination: | 74.0514° |
| perigee height: | 755 km |
| apogee height: | 780 km |
| right ascension of ascending node: | 173.7959° |
| argument of perigee: | 303.3495° |
| revolutions per day: | 14.37331191 |
| mean anomaly at epoch: | 56.5989° |
| orbit number at epoch: | 22327 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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