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 65644U 26145.47843934 +.00000000 +00000-0 +71853-3 0 00005
2 65644 53.1600 310.6934 0000973 77.0177 283.0932 15.30241570 01
| Epoch (UTC): | 25 May 2026 11:28:57 |
| Eccentricity: | 0.0000973 |
| inclination: | 53.1600° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 310.6934° |
| argument of perigee: | 77.0177° |
| revolutions per day: | 15.30241570 |
| mean anomaly at epoch: | 283.0932° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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