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 40014U 14033E 23336.89069112 .00007078 00000-0 54566-3 0 9994
2 40014 98.1526 3.6657 0036585 71.6502 288.8695 15.01416963516012
| Epoch (UTC): | 02 December 2023 21:22:35 |
| Eccentricity: | 0.0036585 |
| inclination: | 98.1526° |
| perigee height: | 537 km |
| apogee height: | 588 km |
| right ascension of ascending node: | 3.6657° |
| argument of perigee: | 71.6502° |
| revolutions per day: | 15.01416963 |
| mean anomaly at epoch: | 288.8695° |
| orbit number at epoch: | 51601 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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