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 23339.88966580 .00004995 00000-0 38639-3 0 9999
2 40014 98.1532 6.8133 0036705 62.1557 298.3377 15.01451034516462
| Epoch (UTC): | 05 December 2023 21:21:07 |
| Eccentricity: | 0.0036705 |
| inclination: | 98.1532° |
| perigee height: | 537 km |
| apogee height: | 588 km |
| right ascension of ascending node: | 6.8133° |
| argument of perigee: | 62.1557° |
| revolutions per day: | 15.01451034 |
| mean anomaly at epoch: | 298.3377° |
| orbit number at epoch: | 51646 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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