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 36089U 09061B 23028.46297347 .00000530 00000-0 14266-3 0 9999
2 36089 98.2883 354.8614 0080535 222.9370 136.5520 14.50165454698845
| Epoch (UTC): | 28 January 2023 11:06:40 |
| Eccentricity: | 0.0080535 |
| inclination: | 98.2883° |
| perigee height: | 668 km |
| apogee height: | 782 km |
| right ascension of ascending node: | 354.8614° |
| argument of perigee: | 222.9370° |
| revolutions per day: | 14.50165454 |
| mean anomaly at epoch: | 136.5520° |
| orbit number at epoch: | 69884 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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