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 65995U 26145.31063316 +.00000000 +00000-0 +40213-4 0 00002
2 65995 50.0004 257.8959 0000820 154.9961 205.0951 13.29327379 03
| Epoch (UTC): | 25 May 2026 07:27:18 |
| Eccentricity: | 0.0000820 |
| inclination: | 50.0004° |
| perigee height: | 1149 km |
| apogee height: | 1150 km |
| right ascension of ascending node: | 257.8959° |
| argument of perigee: | 154.9961° |
| revolutions per day: | 13.29327379 |
| mean anomaly at epoch: | 205.0951° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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