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 65835U 26145.27394102 +.00000000 +00000-0 +58395-3 0 00009
2 65835 53.1575 92.9833 0001154 88.6422 271.4711 15.30212389 07
| Epoch (UTC): | 25 May 2026 06:34:28 |
| Eccentricity: | 0.0001154 |
| inclination: | 53.1575° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 92.9833° |
| argument of perigee: | 88.6422° |
| revolutions per day: | 15.30212389 |
| mean anomaly at epoch: | 271.4711° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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