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 42768U 17036D 23091.33958476 .18586469 24030-5 37696-3 0 9999
2 42768 97.1364 140.8026 0010106 274.9098 85.1051 16.46436138321847
| Epoch (UTC): | 01 April 2023 08:09:00 |
| Eccentricity: | 0.0010106 |
| inclination: | 97.1364° |
| perigee height: | 142 km |
| apogee height: | 155 km |
| right ascension of ascending node: | 140.8026° |
| argument of perigee: | 274.9098° |
| revolutions per day: | 16.46436138 |
| mean anomaly at epoch: | 85.1051° |
| orbit number at epoch: | 32184 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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