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 00029U 60002B 23089.56149914 .00001675 00000-0 27466-3 0 9997
2 00029 48.3792 191.7673 0024464 261.5826 98.2313 14.75166445368499
| Epoch (UTC): | 30 March 2023 13:28:33 |
| Eccentricity: | 0.0024464 |
| inclination: | 48.3792° |
| perigee height: | 627 km |
| apogee height: | 662 km |
| right ascension of ascending node: | 191.7673° |
| argument of perigee: | 261.5826° |
| revolutions per day: | 14.75166445 |
| mean anomaly at epoch: | 98.2313° |
| orbit number at epoch: | 36849 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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