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 16116U 85092B 23273.29971069 -.00000074 00000-0 00000+0 0 9990
2 16116 14.8102 354.8085 0006209 160.4185 229.0189 0.99322128 16068
| Epoch (UTC): | 30 September 2023 07:11:35 |
| Eccentricity: | 0.0006209 |
| inclination: | 14.8102° |
| perigee height: | 36028 km |
| apogee height: | 36081 km |
| right ascension of ascending node: | 354.8085° |
| argument of perigee: | 160.4185° |
| revolutions per day: | 0.99322128 |
| mean anomaly at epoch: | 229.0189° |
| orbit number at epoch: | 1606 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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