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 42792U 17036AD 23289.73389548 .09781629 23598-5 10320-2 0 9994
2 42792 97.0969 333.1645 0009033 260.0160 100.0120 16.37602079352297
| Epoch (UTC): | 16 October 2023 17:36:48 |
| Eccentricity: | 0.0009033 |
| inclination: | 97.0969° |
| perigee height: | 166 km |
| apogee height: | 178 km |
| right ascension of ascending node: | 333.1645° |
| argument of perigee: | 260.0160° |
| revolutions per day: | 16.37602079 |
| mean anomaly at epoch: | 100.0120° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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