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 16182U 85097B 23154.30508838 .00000134 00000-0 91566-4 0 9996
2 16182 71.0017 107.2557 0007925 340.7624 171.4176 14.16336644944149
| Epoch (UTC): | 03 June 2023 07:19:19 |
| Eccentricity: | 0.0007925 |
| inclination: | 71.0017° |
| perigee height: | 832 km |
| apogee height: | 843 km |
| right ascension of ascending node: | 107.2557° |
| argument of perigee: | 340.7624° |
| revolutions per day: | 14.16336644 |
| mean anomaly at epoch: | 171.4176° |
| orbit number at epoch: | 94414 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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