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 31792U 07029A 25142.55698075 .00000119 00000-0 89808-4 0 9997
2 31792 70.9348 94.4796 0005665 289.5980 70.4529 14.12846653922973
| Epoch (UTC): | 22 May 2025 13:22:03 |
| Eccentricity: | 0.0005665 |
| inclination: | 70.9348° |
| perigee height: | 845 km |
| apogee height: | 854 km |
| right ascension of ascending node: | 94.4796° |
| argument of perigee: | 289.5980° |
| revolutions per day: | 14.12846653 |
| mean anomaly at epoch: | 70.4529° |
| orbit number at epoch: | 92297 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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