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 00046U 60007B 25173.27843373 .00000283 00000-0 73082-4 0 9995
2 00046 66.6877 128.7814 0200454 205.7467 153.3562 14.54007259404661
| Epoch (UTC): | 22 June 2025 06:40:56 |
| Eccentricity: | 0.0200454 |
| inclination: | 66.6877° |
| perigee height: | 570 km |
| apogee height: | 855 km |
| right ascension of ascending node: | 128.7814° |
| argument of perigee: | 205.7467° |
| revolutions per day: | 14.54007259 |
| mean anomaly at epoch: | 153.3562° |
| orbit number at epoch: | 40466 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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