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 00045U 60007A 25346.83782567 .00000552 00000-0 15735-3 0 9994
2 00045 66.6925 133.0745 0255642 294.5373 62.9274 14.35781934353292
| Epoch (UTC): | 12 December 2025 20:06:28 |
| Eccentricity: | 0.0255642 |
| inclination: | 66.6925° |
| perigee height: | 589 km |
| apogee height: | 955 km |
| right ascension of ascending node: | 133.0745° |
| argument of perigee: | 294.5373° |
| revolutions per day: | 14.35781934 |
| mean anomaly at epoch: | 62.9274° |
| orbit number at epoch: | 35329 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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