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 14208U 83075B 22228.87730083 .00002097 00000-0 12096-3 0 9999
2 14208 97.4870 202.8991 0039045 101.6643 258.8974 15.12825691132149
| Epoch (UTC): | 16 August 2022 21:03:18 |
| Eccentricity: | 0.0039045 |
| inclination: | 97.4870° |
| perigee height: | 500 km |
| apogee height: | 554 km |
| right ascension of ascending node: | 202.8991° |
| argument of perigee: | 101.6643° |
| revolutions per day: | 15.12825691 |
| mean anomaly at epoch: | 258.8974° |
| orbit number at epoch: | 13214 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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