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 37931U 26145.02615561 +.00000000 +00000-0 +66235-4 0 00006
2 37931 98.6959 164.0250 0022286 211.3081 203.3507 14.31118297 02
| Epoch (UTC): | 25 May 2026 00:37:39 |
| Eccentricity: | 0.0022286 |
| inclination: | 98.6959° |
| perigee height: | 772 km |
| apogee height: | 804 km |
| right ascension of ascending node: | 164.0250° |
| argument of perigee: | 211.3081° |
| revolutions per day: | 14.31118297 |
| mean anomaly at epoch: | 203.3507° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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