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 10489U 77108A 23272.14935311 -.00000099 00000-0 00000+0 0 9996
2 10489 7.5693 292.6725 0007555 82.6322 116.9133 1.00385520127314
| Epoch (UTC): | 29 September 2023 03:35:04 |
| Eccentricity: | 0.0007555 |
| inclination: | 7.5693° |
| perigee height: | 35722 km |
| apogee height: | 35786 km |
| right ascension of ascending node: | 292.6725° |
| argument of perigee: | 82.6322° |
| revolutions per day: | 1.00385520 |
| mean anomaly at epoch: | 116.9133° |
| orbit number at epoch: | 12731 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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