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 23153.30740490 .00000064 00000-0 56477-4 0 9991
2 16182 71.0016 109.3552 0007877 342.0544 124.6481 14.16336327944000
| Epoch (UTC): | 02 June 2023 07:22:39 |
| Eccentricity: | 0.0007877 |
| inclination: | 71.0016° |
| perigee height: | 832 km |
| apogee height: | 843 km |
| right ascension of ascending node: | 109.3552° |
| argument of perigee: | 342.0544° |
| revolutions per day: | 14.16336327 |
| mean anomaly at epoch: | 124.6481° |
| orbit number at epoch: | 94400 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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