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 31708U 07027C 25184.95571157 0.00000128 00000-0 13156-3 0 08
2 31708 63.3748 137.9439 0437346 22.7298 337.2726 13.40965892 02
| Epoch (UTC): | 03 July 2025 22:56:13 |
| Eccentricity: | 0.0437346 |
| inclination: | 63.3748° |
| perigee height: | 778 km |
| apogee height: | 1433 km |
| right ascension of ascending node: | 137.9439° |
| argument of perigee: | 22.7298° |
| revolutions per day: | 13.40965892 |
| mean anomaly at epoch: | 337.2726° |
| 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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