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 65975U 26145.49399022 +.00000000 +00000-0 +16266-3 0 00005
2 65975 81.3017 232.8740 0001233 107.8721 252.2569 13.82038341 09
| Epoch (UTC): | 25 May 2026 11:51:20 |
| Eccentricity: | 0.0001233 |
| inclination: | 81.3017° |
| perigee height: | 956 km |
| apogee height: | 958 km |
| right ascension of ascending node: | 232.8740° |
| argument of perigee: | 107.8721° |
| revolutions per day: | 13.82038341 |
| mean anomaly at epoch: | 252.2569° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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