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 16369U 85116B 23152.46124807 .00000197 00000-0 18383-3 0 9994
2 16369 82.9361 170.4422 0036068 188.9384 281.3537 13.76956388881013
| Epoch (UTC): | 01 June 2023 11:04:11 |
| Eccentricity: | 0.0036068 |
| inclination: | 82.9361° |
| perigee height: | 948 km |
| apogee height: | 1001 km |
| right ascension of ascending node: | 170.4422° |
| argument of perigee: | 188.9384° |
| revolutions per day: | 13.76956388 |
| mean anomaly at epoch: | 281.3537° |
| orbit number at epoch: | 88101 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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