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 25194.10677926 0.00000000 00000-0 00000-0 0 09
2 31797 98.1293 261.0037 0003000 195.3932 164.6067 15.27566246 09
| Epoch (UTC): | 13 July 2025 02:33:45 |
| Eccentricity: | 0.0003000 |
| inclination: | 98.1293° |
| perigee height: | 481 km |
| apogee height: | 485 km |
| right ascension of ascending node: | 261.0037° |
| argument of perigee: | 195.3932° |
| revolutions per day: | 15.27566246 |
| mean anomaly at epoch: | 164.6067° |
| 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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