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 65993U 26145.52012675 +.00000000 +00000-0 +10326-3 0 00006
2 65993 81.3021 233.2181 0001257 114.3375 245.7910 13.79141736 08
| Epoch (UTC): | 25 May 2026 12:28:58 |
| Eccentricity: | 0.0001257 |
| inclination: | 81.3021° |
| perigee height: | 966 km |
| apogee height: | 968 km |
| right ascension of ascending node: | 233.2181° |
| argument of perigee: | 114.3375° |
| revolutions per day: | 13.79141736 |
| mean anomaly at epoch: | 245.7910° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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