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 31699U 07026B 24280.87462544 .00004092 00000-0 58900-3 0 9999
2 31699 97.4528 315.0980 0340568 122.1100 47.9622 14.44176242910212
| Epoch (UTC): | 06 October 2024 20:59:27 |
| Eccentricity: | 0.0340568 |
| inclination: | 97.4528° |
| perigee height: | 502 km |
| apogee height: | 987 km |
| right ascension of ascending node: | 315.0980° |
| argument of perigee: | 122.1100° |
| revolutions per day: | 14.44176242 |
| mean anomaly at epoch: | 47.9622° |
| orbit number at epoch: | 91021 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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