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 is defined by the following mean orbital elements,
1 39731U 26145.61038492 +.00000000 +00000-0 +12308-3 0 00004
2 39731 98.3206 218.6185 0001569 86.0387 274.0983 14.42070183 00
| Epoch (UTC): | 25 May 2026 14:38:57 |
| Eccentricity: | 0.0001569 |
| inclination: | 98.3206° |
| perigee height: | 751 km |
| apogee height: | 753 km |
| right ascension of ascending node: | 218.6185° |
| argument of perigee: | 86.0387° |
| revolutions per day: | 14.42070183 |
| mean anomaly at epoch: | 274.0983° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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