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 36582U 10021B 22225.69294649 .00000069 00000-0 00000-0 0 9995
2 36582 0.0211 140.7965 0002335 11.8902 72.0845 1.00268177 44888
| Epoch (UTC): | 13 August 2022 16:37:50 |
| Eccentricity: | 0.0002335 |
| inclination: | 0.0211° |
| perigee height: | 35777 km |
| apogee height: | 35797 km |
| right ascension of ascending node: | 140.7965° |
| argument of perigee: | 11.8902° |
| revolutions per day: | 1.00268177 |
| mean anomaly at epoch: | 72.0845° |
| orbit number at epoch: | 4488 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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