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 00020U 59007A 25338.99677140 .00003080 00000-0 12414-2 0 9992
2 00020 33.3410 246.0086 1639284 92.6592 286.1867 11.61570743462027
| Epoch (UTC): | 04 December 2025 23:55:21 |
| Eccentricity: | 0.1639284 |
| inclination: | 33.3410° |
| perigee height: | 507 km |
| apogee height: | 3208 km |
| right ascension of ascending node: | 246.0086° |
| argument of perigee: | 92.6592° |
| revolutions per day: | 11.61570743 |
| mean anomaly at epoch: | 286.1867° |
| orbit number at epoch: | 46202 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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