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 65575U 26145.65197110 +.00000000 +00000-0 +16850-3 0 00002
2 65575 81.3048 31.4177 0008261 253.6884 106.3365 13.85035251 07
| Epoch (UTC): | 25 May 2026 15:38:50 |
| Eccentricity: | 0.0008261 |
| inclination: | 81.3048° |
| perigee height: | 940 km |
| apogee height: | 952 km |
| right ascension of ascending node: | 31.4177° |
| argument of perigee: | 253.6884° |
| revolutions per day: | 13.85035251 |
| mean anomaly at epoch: | 106.3365° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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