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 00116U 61015A 23091.85644945 .00000122 00000-0 15238-3 0 9998
2 00116 66.8089 238.4486 0074519 9.9606 350.2930 13.91900721133527
| Epoch (UTC): | 01 April 2023 20:33:17 |
| Eccentricity: | 0.0074519 |
| inclination: | 66.8089° |
| perigee height: | 867 km |
| apogee height: | 976 km |
| right ascension of ascending node: | 238.4486° |
| argument of perigee: | 9.9606° |
| revolutions per day: | 13.91900721 |
| mean anomaly at epoch: | 350.2930° |
| orbit number at epoch: | 13352 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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