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 is defined by the following mean orbital elements,
1 42788U 17036Z 23278.90222119 .18188609 24489-5 22826-3 0 9990
2 42788 97.0954 322.8452 0011132 248.8258 111.1858 16.49176567350708
| Epoch (UTC): | 05 October 2023 21:39:11 |
| Eccentricity: | 0.0011132 |
| inclination: | 97.0954° |
| perigee height: | 134 km |
| apogee height: | 149 km |
| right ascension of ascending node: | 322.8452° |
| argument of perigee: | 248.8258° |
| revolutions per day: | 16.49176567 |
| mean anomaly at epoch: | 111.1858° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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