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 37765U 26145.30053307 +.00000000 +00000-0 +95409-4 0 00001
2 37765 98.2651 35.2129 0010144 342.0939 133.8481 14.64450538 01
| Epoch (UTC): | 25 May 2026 07:12:46 |
| Eccentricity: | 0.0010144 |
| inclination: | 98.2651° |
| perigee height: | 672 km |
| apogee height: | 686 km |
| right ascension of ascending node: | 35.2129° |
| argument of perigee: | 342.0939° |
| revolutions per day: | 14.64450538 |
| mean anomaly at epoch: | 133.8481° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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