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 15333U 84106A 25132.52421505 -.00000182 00000-0 -70050-4 0 9990
2 15333 71.0252 167.4351 0017746 137.6028 222.6470 14.14454290 96083
| Epoch (UTC): | 12 May 2025 12:34:52 |
| Eccentricity: | 0.0017746 |
| inclination: | 71.0252° |
| perigee height: | 831 km |
| apogee height: | 857 km |
| right ascension of ascending node: | 167.4351° |
| argument of perigee: | 137.6028° |
| revolutions per day: | 14.14454290 |
| mean anomaly at epoch: | 222.6470° |
| orbit number at epoch: | 9608 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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