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 65888U 26145.05353562 +.00000000 +00000-0 +57374-3 0 00004
2 65888 53.1603 16.8142 0001259 83.0918 277.0226 15.30198622 06
| Epoch (UTC): | 25 May 2026 01:17:05 |
| Eccentricity: | 0.0001259 |
| inclination: | 53.1603° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 16.8142° |
| argument of perigee: | 83.0918° |
| revolutions per day: | 15.30198622 |
| mean anomaly at epoch: | 277.0226° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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