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 00005U 58002B 23028.74518793 .00000154 00000-0 19226-3 0 9992
2 00005 34.2491 165.0939 1846034 331.7015 19.4298 10.85055844309015
| Epoch (UTC): | 28 January 2023 17:53:04 |
| Eccentricity: | 0.1846034 |
| inclination: | 34.2491° |
| perigee height: | 649 km |
| apogee height: | 3831 km |
| right ascension of ascending node: | 165.0939° |
| argument of perigee: | 331.7015° |
| revolutions per day: | 10.85055844 |
| mean anomaly at epoch: | 19.4298° |
| orbit number at epoch: | 30901 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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