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 23340.55609617 .00004320 00000-0 33486-3 0 9997
2 40014 98.1533 7.5128 0036732 60.0659 300.4203 15.01456532516567
| Epoch (UTC): | 06 December 2023 13:20:46 |
| Eccentricity: | 0.0036732 |
| inclination: | 98.1533° |
| perigee height: | 537 km |
| apogee height: | 588 km |
| right ascension of ascending node: | 7.5128° |
| argument of perigee: | 60.0659° |
| revolutions per day: | 15.01456532 |
| mean anomaly at epoch: | 300.4203° |
| orbit number at epoch: | 51656 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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