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 09613U 76122B 23152.41997089 .00000185 00000-0 17052-3 0 9999
2 09613 82.9529 336.5957 0029146 314.5024 45.3751 13.77560303334533
| Epoch (UTC): | 01 June 2023 10:04:45 |
| Eccentricity: | 0.0029146 |
| inclination: | 82.9529° |
| perigee height: | 951 km |
| apogee height: | 994 km |
| right ascension of ascending node: | 336.5957° |
| argument of perigee: | 314.5024° |
| revolutions per day: | 13.77560303 |
| mean anomaly at epoch: | 45.3751° |
| orbit number at epoch: | 33453 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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