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 65228U 26145.61697546 +.00000000 +00000-0 +77369-4 0 00004
2 65228 86.5001 21.1431 0001635 87.3531 272.7790 13.24408870 00
| Epoch (UTC): | 25 May 2026 14:48:26 |
| Eccentricity: | 0.0001635 |
| inclination: | 86.5001° |
| perigee height: | 1167 km |
| apogee height: | 1169 km |
| right ascension of ascending node: | 21.1431° |
| argument of perigee: | 87.3531° |
| revolutions per day: | 13.24408870 |
| mean anomaly at epoch: | 272.7790° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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