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 14506U 83113A 24277.20957193 .00001899 00000-0 76446-3 0 9997
2 14506 98.3445 74.9074 0009864 268.0971 264.6623 14.29134850126917
| Epoch (UTC): | 03 October 2024 05:01:47 |
| Eccentricity: | 0.0009864 |
| inclination: | 98.3445° |
| perigee height: | 787 km |
| apogee height: | 802 km |
| right ascension of ascending node: | 74.9074° |
| argument of perigee: | 268.0971° |
| revolutions per day: | 14.29134850 |
| mean anomaly at epoch: | 264.6623° |
| orbit number at epoch: | 12691 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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