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 00050U 60009B 23089.56812593 -.00000077 00000-0 87853-4 0 9991
2 00050 47.2300 207.5675 0113648 114.3645 246.9056 12.20128094794283
| Epoch (UTC): | 30 March 2023 13:38:06 |
| Eccentricity: | 0.0113648 |
| inclination: | 47.2300° |
| perigee height: | 1501 km |
| apogee height: | 1682 km |
| right ascension of ascending node: | 207.5675° |
| argument of perigee: | 114.3645° |
| revolutions per day: | 12.20128094 |
| mean anomaly at epoch: | 246.9056° |
| orbit number at epoch: | 79428 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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