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 65999U 26145.28557646 +.00000000 +00000-0 +50625-4 0 00004
2 65999 50.0015 257.7911 0000923 151.5749 208.5174 13.29326395 09
| Epoch (UTC): | 25 May 2026 06:51:13 |
| Eccentricity: | 0.0000923 |
| inclination: | 50.0015° |
| perigee height: | 1149 km |
| apogee height: | 1150 km |
| right ascension of ascending node: | 257.7911° |
| argument of perigee: | 151.5749° |
| revolutions per day: | 13.29326395 |
| mean anomaly at epoch: | 208.5174° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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