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 65740U 26145.55431588 +.00000000 +00000-0 +47437-3 0 00000
2 65740 53.1583 335.7408 0001653 98.8854 261.2334 15.30209462 09
| Epoch (UTC): | 25 May 2026 13:18:12 |
| Eccentricity: | 0.0001653 |
| inclination: | 53.1583° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 335.7408° |
| argument of perigee: | 98.8854° |
| revolutions per day: | 15.30209462 |
| mean anomaly at epoch: | 261.2334° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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