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 17160U 86093B 23156.62209554 .00000088 00000-0 76520-4 0 9991
2 17160 82.9288 247.3980 0038673 192.5433 280.0419 13.74717477832028
| Epoch (UTC): | 05 June 2023 14:55:49 |
| Eccentricity: | 0.0038673 |
| inclination: | 82.9288° |
| perigee height: | 954 km |
| apogee height: | 1011 km |
| right ascension of ascending node: | 247.3980° |
| argument of perigee: | 192.5433° |
| revolutions per day: | 13.74717477 |
| mean anomaly at epoch: | 280.0419° |
| orbit number at epoch: | 83202 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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