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 37392U 26145.43165093 +.00000000 +00000-0 +00000-0 0 00006
2 37392 1.7496 82.8877 0003909 343.1940 300.6189 1.00270638 02
| Epoch (UTC): | 25 May 2026 10:21:34 |
| Eccentricity: | 0.0003909 |
| inclination: | 1.7496° |
| perigee height: | 35770 km |
| apogee height: | 35803 km |
| right ascension of ascending node: | 82.8877° |
| argument of perigee: | 343.1940° |
| revolutions per day: | 1.00270638 |
| mean anomaly at epoch: | 300.6189° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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