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 40057U 14034E 24340.55878515 .00010390 00000-0 10887-2 0 9994
2 40057 98.3154 204.2121 0007983 315.1552 44.9018 14.89750717563187
| Epoch (UTC): | 05 December 2024 13:24:39 |
| Eccentricity: | 0.0007983 |
| inclination: | 98.3154° |
| perigee height: | 593 km |
| apogee height: | 604 km |
| right ascension of ascending node: | 204.2121° |
| argument of perigee: | 315.1552° |
| revolutions per day: | 14.89750717 |
| mean anomaly at epoch: | 44.9018° |
| orbit number at epoch: | 56318 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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