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 00045U 60007A 23337.31664289 .00000567 00000-0 16918-3 0 9995
2 00045 66.6944 289.1200 0246509 116.1679 246.5000 14.34457883247035
| Epoch (UTC): | 03 December 2023 07:35:57 |
| Eccentricity: | 0.0246509 |
| inclination: | 66.6944° |
| perigee height: | 600 km |
| apogee height: | 953 km |
| right ascension of ascending node: | 289.1200° |
| argument of perigee: | 116.1679° |
| revolutions per day: | 14.34457883 |
| mean anomaly at epoch: | 246.5000° |
| orbit number at epoch: | 24703 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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