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 23150.80266391 .00000182 00000-0 16791-3 0 9990
2 16369 82.9362 171.6757 0035964 193.6199 339.6432 13.76955749880783
| Epoch (UTC): | 30 May 2023 19:15:50 |
| Eccentricity: | 0.0035964 |
| inclination: | 82.9362° |
| perigee height: | 948 km |
| apogee height: | 1001 km |
| right ascension of ascending node: | 171.6757° |
| argument of perigee: | 193.6199° |
| revolutions per day: | 13.76955749 |
| mean anomaly at epoch: | 339.6432° |
| orbit number at epoch: | 88078 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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