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 27909U 84069AB 22272.06342281 .00000131 00000-0 17395-3 0 9998
2 27909 65.0463 157.5362 0030319 125.5011 234.8889 13.91561233463204
| Epoch (UTC): | 29 September 2022 01:31:19 |
| Eccentricity: | 0.0030319 |
| inclination: | 65.0463° |
| perigee height: | 901 km |
| apogee height: | 945 km |
| right ascension of ascending node: | 157.5362° |
| argument of perigee: | 125.5011° |
| revolutions per day: | 13.91561233 |
| mean anomaly at epoch: | 234.8889° |
| orbit number at epoch: | 46320 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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