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 37265U 26145.45561464 +.00000000 +00000-0 +00000-0 0 00009
2 37265 0.0174 293.9019 0002251 129.3828 143.6592 1.00271311 09
| Epoch (UTC): | 25 May 2026 10:56:05 |
| Eccentricity: | 0.0002251 |
| inclination: | 0.0174° |
| perigee height: | 35777 km |
| apogee height: | 35796 km |
| right ascension of ascending node: | 293.9019° |
| argument of perigee: | 129.3828° |
| revolutions per day: | 1.00271311 |
| mean anomaly at epoch: | 143.6592° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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