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 14506U 83113A 24358.05613920 .00000666 00000-0 27790-3 0 9996
2 14506 98.3493 152.3650 0011443 34.5237 75.5915 14.29315542138463
| Epoch (UTC): | 23 December 2024 01:20:50 |
| Eccentricity: | 0.0011443 |
| inclination: | 98.3493° |
| perigee height: | 786 km |
| apogee height: | 802 km |
| right ascension of ascending node: | 152.3650° |
| argument of perigee: | 34.5237° |
| revolutions per day: | 14.29315542 |
| mean anomaly at epoch: | 75.5915° |
| orbit number at epoch: | 13846 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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