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 40057U 14034E 25073.89710724 .00010981 00000-0 10947-2 0 9995
2 40057 98.3066 308.7710 0008269 350.5017 9.6042 14.91737999577988
| Epoch (UTC): | 14 March 2025 21:31:50 |
| Eccentricity: | 0.0008269 |
| inclination: | 98.3066° |
| perigee height: | 587 km |
| apogee height: | 598 km |
| right ascension of ascending node: | 308.7710° |
| argument of perigee: | 350.5017° |
| revolutions per day: | 14.91737999 |
| mean anomaly at epoch: | 9.6042° |
| orbit number at epoch: | 57798 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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