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 03230U 68040B 24357.84500287 .00006171 00000-0 50881-3 0 9991
2 03230 74.0321 133.7750 0025587 71.8604 288.5365 14.98988763 23708
| Epoch (UTC): | 22 December 2024 20:16:48 |
| Eccentricity: | 0.0025587 |
| inclination: | 74.0321° |
| perigee height: | 552 km |
| apogee height: | 588 km |
| right ascension of ascending node: | 133.7750° |
| argument of perigee: | 71.8604° |
| revolutions per day: | 14.98988763 |
| mean anomaly at epoch: | 288.5365° |
| orbit number at epoch: | 2370 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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