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 42016U 17008BW 23204.99452570 .06708397 23815-5 10367-2 0 9994
2 42016 97.1850 278.5320 0015441 258.3858 101.5706 16.33716732359282
| Epoch (UTC): | 23 July 2023 23:52:07 |
| Eccentricity: | 0.0015441 |
| inclination: | 97.1850° |
| perigee height: | 172 km |
| apogee height: | 193 km |
| right ascension of ascending node: | 278.5320° |
| argument of perigee: | 258.3858° |
| revolutions per day: | 16.33716732 |
| mean anomaly at epoch: | 101.5706° |
| orbit number at epoch: | 35928 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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