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 31766U 99025CFR 24354.23666681 .00000582 00000-0 37879-3 0 9996
2 31766 98.8071 356.1953 0074154 215.0548 144.5727 14.04994048905643
| Epoch (UTC): | 19 December 2024 05:40:48 |
| Eccentricity: | 0.0074154 |
| inclination: | 98.8071° |
| perigee height: | 823 km |
| apogee height: | 930 km |
| right ascension of ascending node: | 356.1953° |
| argument of perigee: | 215.0548° |
| revolutions per day: | 14.04994048 |
| mean anomaly at epoch: | 144.5727° |
| orbit number at epoch: | 90564 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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