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 23158.11169973 .00000159 00000-0 65264-4 0 9990
2 00045 66.6954 41.8685 0260842 246.6436 110.7031 14.34220993221333
| Epoch (UTC): | 07 June 2023 02:40:50 |
| Eccentricity: | 0.0260842 |
| inclination: | 66.6954° |
| perigee height: | 591 km |
| apogee height: | 964 km |
| right ascension of ascending node: | 41.8685° |
| argument of perigee: | 246.6436° |
| revolutions per day: | 14.34220993 |
| mean anomaly at epoch: | 110.7031° |
| orbit number at epoch: | 22133 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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