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 37933U 26145.60467946 +.00000000 +00000-0 +00000-0 0 00008
2 37933 0.0300 269.8472 0001564 143.0130 153.5194 1.00270045 03
| Epoch (UTC): | 25 May 2026 14:30:44 |
| Eccentricity: | 0.0001564 |
| inclination: | 0.0300° |
| perigee height: | 35780 km |
| apogee height: | 35794 km |
| right ascension of ascending node: | 269.8472° |
| argument of perigee: | 143.0130° |
| revolutions per day: | 1.00270045 |
| mean anomaly at epoch: | 153.5194° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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