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 30312U 99025ZZ 24277.11714795 .00036246 00000-0 12541-1 0 9996
2 30312 98.8954 333.5758 0012757 77.8684 343.8038 14.35490960916556
| Epoch (UTC): | 03 October 2024 02:48:41 |
| Eccentricity: | 0.0012757 |
| inclination: | 98.8954° |
| perigee height: | 764 km |
| apogee height: | 782 km |
| right ascension of ascending node: | 333.5758° |
| argument of perigee: | 77.8684° |
| revolutions per day: | 14.35490960 |
| mean anomaly at epoch: | 343.8038° |
| orbit number at epoch: | 91655 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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