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 25136.85356487 0.00000000 00000-0 00000-0 0 03
2 31797 98.1373 198.6719 0006335 34.0069 325.9929 15.27586246 05
| Epoch (UTC): | 16 May 2025 20:29:08 |
| Eccentricity: | 0.0006335 |
| inclination: | 98.1373° |
| perigee height: | 478 km |
| apogee height: | 487 km |
| right ascension of ascending node: | 198.6719° |
| argument of perigee: | 34.0069° |
| revolutions per day: | 15.27586246 |
| mean anomaly at epoch: | 325.9929° |
| 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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