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 25118.43640919 .00005871 00000-0 68166-3 0 9992
2 40012 97.7372 275.8222 0047628 354.8690 5.2031 14.84933038584544
| Epoch (UTC): | 28 April 2025 10:28:25 |
| Eccentricity: | 0.0047628 |
| inclination: | 97.7372° |
| perigee height: | 580 km |
| apogee height: | 647 km |
| right ascension of ascending node: | 275.8222° |
| argument of perigee: | 354.8690° |
| revolutions per day: | 14.84933038 |
| mean anomaly at epoch: | 5.2031° |
| orbit number at epoch: | 58454 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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