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 27386U 02009A 21106.81200440 .00000027 00000-0 22486-4 0 9991
2 27386 98.1481 104.0215 0001378 87.5962 40.0867 14.38021090 2216
| Epoch (UTC): | 16 April 2021 19:29:17 |
| Eccentricity: | 0.0001378 |
| inclination: | 98.1481° |
| perigee height: | 764 km |
| apogee height: | 766 km |
| right ascension of ascending node: | 104.0215° |
| argument of perigee: | 87.5962° |
| revolutions per day: | 14.38021090 |
| mean anomaly at epoch: | 40.0867° |
| orbit number at epoch: | 221 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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