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 20491U 90013D 23337.18448040 .00000170 00000-0 37923-3 0 9991
2 20491 99.0691 49.7789 0468415 173.3904 187.3684 13.03645506608230
| Epoch (UTC): | 03 December 2023 04:25:39 |
| Eccentricity: | 0.0468415 |
| inclination: | 99.0691° |
| perigee height: | 890 km |
| apogee height: | 1605 km |
| right ascension of ascending node: | 49.7789° |
| argument of perigee: | 173.3904° |
| revolutions per day: | 13.03645506 |
| mean anomaly at epoch: | 187.3684° |
| orbit number at epoch: | 60823 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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