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 23334.82468082 .00008309 00000-0 64015-3 0 9992
2 40014 98.1519 1.4977 0036493 78.2456 282.2858 15.01382284515717
| Epoch (UTC): | 30 November 2023 19:47:32 |
| Eccentricity: | 0.0036493 |
| inclination: | 98.1519° |
| perigee height: | 537 km |
| apogee height: | 588 km |
| right ascension of ascending node: | 1.4977° |
| argument of perigee: | 78.2456° |
| revolutions per day: | 15.01382284 |
| mean anomaly at epoch: | 282.2858° |
| orbit number at epoch: | 51571 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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