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 31262U 99025BMU 23270.16246304 .00004531 00000-0 25781-2 0 9997
2 31262 99.0495 335.3837 0063910 216.5384 199.8892 14.09288672842986
| Epoch (UTC): | 27 September 2023 03:53:56 |
| Eccentricity: | 0.0063910 |
| inclination: | 99.0495° |
| perigee height: | 815 km |
| apogee height: | 908 km |
| right ascension of ascending node: | 335.3837° |
| argument of perigee: | 216.5384° |
| revolutions per day: | 14.09288672 |
| mean anomaly at epoch: | 199.8892° |
| orbit number at epoch: | 84298 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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