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 40012U 14033C 24260.92603117 .00007788 00000-0 98392-3 0 9995
2 40012 97.7130 59.7334 0051498 6.8532 353.3374 14.81198383551418
| Epoch (UTC): | 16 September 2024 22:13:29 |
| Eccentricity: | 0.0051498 |
| inclination: | 97.7130° |
| perigee height: | 589 km |
| apogee height: | 661 km |
| right ascension of ascending node: | 59.7334° |
| argument of perigee: | 6.8532° |
| revolutions per day: | 14.81198383 |
| mean anomaly at epoch: | 353.3374° |
| orbit number at epoch: | 55141 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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