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 65635U 26145.47527313 +.00000000 +00000-0 +73553-3 0 00004
2 65635 53.1585 310.6714 0001436 102.2791 257.8371 15.30215720 01
| Epoch (UTC): | 25 May 2026 11:24:23 |
| Eccentricity: | 0.0001436 |
| inclination: | 53.1585° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 310.6714° |
| argument of perigee: | 102.2791° |
| revolutions per day: | 15.30215720 |
| mean anomaly at epoch: | 257.8371° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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