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 29812U 99025DE 24358.08811917 .00003682 00000-0 22999-2 0 9996
2 29812 98.3876 210.2499 0143423 248.4220 265.3522 14.00340922912261
| Epoch (UTC): | 23 December 2024 02:06:53 |
| Eccentricity: | 0.0143423 |
| inclination: | 98.3876° |
| perigee height: | 788 km |
| apogee height: | 997 km |
| right ascension of ascending node: | 210.2499° |
| argument of perigee: | 248.4220° |
| revolutions per day: | 14.00340922 |
| mean anomaly at epoch: | 265.3522° |
| orbit number at epoch: | 91226 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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