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 10306U 77065DC 24357.51995926 .00008058 00000-0 20274-2 0 9990
2 10306 29.1103 71.3576 0667442 265.9165 86.4899 13.64479580316977
| Epoch (UTC): | 22 December 2024 12:28:44 |
| Eccentricity: | 0.0667442 |
| inclination: | 29.1103° |
| perigee height: | 526 km |
| apogee height: | 1513 km |
| right ascension of ascending node: | 71.3576° |
| argument of perigee: | 265.9165° |
| revolutions per day: | 13.64479580 |
| mean anomaly at epoch: | 86.4899° |
| orbit number at epoch: | 31697 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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