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 22145.86114149 .00000048 00000-0 95308-4 0 9990
2 00116 66.8100 278.8082 0081382 236.1256 123.2062 13.91829644 90241
| Epoch (UTC): | 25 May 2022 20:40:02 |
| Eccentricity: | 0.0081382 |
| inclination: | 66.8100° |
| perigee height: | 863 km |
| apogee height: | 981 km |
| right ascension of ascending node: | 278.8082° |
| argument of perigee: | 236.1256° |
| revolutions per day: | 13.91829644 |
| mean anomaly at epoch: | 123.2062° |
| orbit number at epoch: | 9024 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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