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 31793U 07029B 25198.78296257 .00000109 00000-0 81108-4 0 9994
2 31793 70.9774 306.1552 0002333 281.4129 243.3371 14.14792753932144
| Epoch (UTC): | 17 July 2025 18:47:27 |
| Eccentricity: | 0.0002333 |
| inclination: | 70.9774° |
| perigee height: | 841 km |
| apogee height: | 845 km |
| right ascension of ascending node: | 306.1552° |
| argument of perigee: | 281.4129° |
| revolutions per day: | 14.14792753 |
| mean anomaly at epoch: | 243.3371° |
| orbit number at epoch: | 93214 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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