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 65909U 26145.06725132 +.00000000 +00000-0 +81291-3 0 00000
2 65909 53.1586 16.8864 0000981 76.8065 283.3045 15.30209031 01
| Epoch (UTC): | 25 May 2026 01:36:50 |
| Eccentricity: | 0.0000981 |
| inclination: | 53.1586° |
| perigee height: | 475 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 16.8864° |
| argument of perigee: | 76.8065° |
| revolutions per day: | 15.30209031 |
| mean anomaly at epoch: | 283.3045° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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