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 37237U 26145.58650177 +.00000000 +00000-0 +00000-0 0 00002
2 37237 5.5887 73.2921 0001356 312.8404 81.9831 1.00272916 06
| Epoch (UTC): | 25 May 2026 14:04:33 |
| Eccentricity: | 0.0001356 |
| inclination: | 5.5887° |
| perigee height: | 35781 km |
| apogee height: | 35792 km |
| right ascension of ascending node: | 73.2921° |
| argument of perigee: | 312.8404° |
| revolutions per day: | 1.00272916 |
| mean anomaly at epoch: | 81.9831° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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