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 44536U 26145.57324078 +.00000000 +00000-0 +43882-3 0 00007
2 44536 97.5505 302.1456 0008896 46.4172 313.7817 15.52671094 01
| Epoch (UTC): | 25 May 2026 13:45:28 |
| Eccentricity: | 0.0008896 |
| inclination: | 97.5505° |
| perigee height: | 403 km |
| apogee height: | 415 km |
| right ascension of ascending node: | 302.1456° |
| argument of perigee: | 46.4172° |
| revolutions per day: | 15.52671094 |
| mean anomaly at epoch: | 313.7817° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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