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 65353U 26145.46430602 +.00000000 +00000-0 +40018-3 0 00004
2 65353 53.1596 171.2895 0000925 78.1041 282.0063 15.30204930 01
| Epoch (UTC): | 25 May 2026 11:08:36 |
| Eccentricity: | 0.0000925 |
| inclination: | 53.1596° |
| perigee height: | 475 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 171.2895° |
| argument of perigee: | 78.1041° |
| revolutions per day: | 15.30204930 |
| mean anomaly at epoch: | 282.0063° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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