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 39975U 87068DB 22225.28944130 .00000464 00000-0 28758-3 0 9993
2 39975 82.5965 222.2105 0101498 202.0685 157.6100 14.00821476418714
| Epoch (UTC): | 13 August 2022 06:56:47 |
| Eccentricity: | 0.0101498 |
| inclination: | 82.5965° |
| perigee height: | 817 km |
| apogee height: | 965 km |
| right ascension of ascending node: | 222.2105° |
| argument of perigee: | 202.0685° |
| revolutions per day: | 14.00821476 |
| mean anomaly at epoch: | 157.6100° |
| orbit number at epoch: | 41871 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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