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 23080.49574066 .00000328 00000-0 10655-3 0 9999
2 00045 66.6928 246.5981 0260539 301.6875 55.9057 14.34135146210206
| Epoch (UTC): | 21 March 2023 11:53:51 |
| Eccentricity: | 0.0260539 |
| inclination: | 66.6928° |
| perigee height: | 591 km |
| apogee height: | 964 km |
| right ascension of ascending node: | 246.5981° |
| argument of perigee: | 301.6875° |
| revolutions per day: | 14.34135146 |
| mean anomaly at epoch: | 55.9057° |
| orbit number at epoch: | 21020 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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