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 31797U 07030A 25244.86651796 0.00010000 00000-0 37029-3 0 00
2 31797 98.1173 316.2998 0005000 309.1998 50.8000 15.27679260 08
| Epoch (UTC): | 01 September 2025 20:47:47 |
| Eccentricity: | 0.0005000 |
| inclination: | 98.1173° |
| perigee height: | 479 km |
| apogee height: | 486 km |
| right ascension of ascending node: | 316.2998° |
| argument of perigee: | 309.1998° |
| revolutions per day: | 15.27679260 |
| mean anomaly at epoch: | 50.8000° |
| orbit number at epoch: | 0 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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