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 42783U 17036U 24117.64658277 .13634305 23923-5 37268-3 0 9999
2 42783 97.0708 157.6240 0010367 256.2840 103.7309 16.44804491381754
| Epoch (UTC): | 26 April 2024 15:31:04 |
| Eccentricity: | 0.0010367 |
| inclination: | 97.0708° |
| perigee height: | 146 km |
| apogee height: | 160 km |
| right ascension of ascending node: | 157.6240° |
| argument of perigee: | 256.2840° |
| revolutions per day: | 16.44804491 |
| mean anomaly at epoch: | 103.7309° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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