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 65695U 26145.55383241 +.00000000 +00000-0 +39110-3 0 00000
2 65695 53.1619 348.5127 0001380 115.1100 245.0045 15.30177528 08
| Epoch (UTC): | 25 May 2026 13:17:31 |
| Eccentricity: | 0.0001380 |
| inclination: | 53.1619° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 348.5127° |
| argument of perigee: | 115.1100° |
| revolutions per day: | 15.30177528 |
| mean anomaly at epoch: | 245.0045° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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