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 65760U 26145.52476671 +.00000000 +00000-0 +50372-3 0 00003
2 65760 53.1603 335.5512 0001481 94.1599 265.9571 15.30209277 00
| Epoch (UTC): | 25 May 2026 12:35:39 |
| Eccentricity: | 0.0001481 |
| inclination: | 53.1603° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 335.5512° |
| argument of perigee: | 94.1599° |
| revolutions per day: | 15.30209277 |
| mean anomaly at epoch: | 265.9571° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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