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 65910U 26145.48380145 +.00000000 +00000-0 +40181-3 0 00002
2 65910 53.1579 169.1217 0000951 82.1965 277.9144 15.30203438 09
| Epoch (UTC): | 25 May 2026 11:36:40 |
| Eccentricity: | 0.0000951 |
| inclination: | 53.1579° |
| perigee height: | 475 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 169.1217° |
| argument of perigee: | 82.1965° |
| revolutions per day: | 15.30203438 |
| mean anomaly at epoch: | 277.9144° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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