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 53662U 26145.66668980 +.00000000 +00000-0 +23430-2 0 00006
2 53662 97.6034 28.4936 0001388 77.6861 338.8367 15.40541024 04
| Epoch (UTC): | 25 May 2026 16:00:01 |
| Eccentricity: | 0.0001388 |
| inclination: | 97.6034° |
| perigee height: | 444 km |
| apogee height: | 445 km |
| right ascension of ascending node: | 28.4936° |
| argument of perigee: | 77.6861° |
| revolutions per day: | 15.40541024 |
| mean anomaly at epoch: | 338.8367° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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