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 30848U 99025AWJ 23333.36542240 .00005377 00000-0 22575-2 0 9993
2 30848 99.0320 126.8538 0048503 333.8793 25.9939 14.25685910866656
| Epoch (UTC): | 29 November 2023 08:46:12 |
| Eccentricity: | 0.0048503 |
| inclination: | 99.0320° |
| perigee height: | 771 km |
| apogee height: | 841 km |
| right ascension of ascending node: | 126.8538° |
| argument of perigee: | 333.8793° |
| revolutions per day: | 14.25685910 |
| mean anomaly at epoch: | 25.9939° |
| orbit number at epoch: | 86665 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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