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 61664U 26145.28302398 +.00000000 +00000-0 +39239-4 0 00009
2 61664 53.1605 95.2252 0001171 93.0260 267.0875 15.31708118 00
| Epoch (UTC): | 25 May 2026 06:47:33 |
| Eccentricity: | 0.0001171 |
| inclination: | 53.1605° |
| perigee height: | 470 km |
| apogee height: | 472 km |
| right ascension of ascending node: | 95.2252° |
| argument of perigee: | 93.0260° |
| revolutions per day: | 15.31708118 |
| mean anomaly at epoch: | 267.0875° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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