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 65991U 26145.52555867 +.00000000 +00000-0 +85871-4 0 00007
2 65991 81.3016 232.5733 0003025 253.5941 106.4884 13.85300692 03
| Epoch (UTC): | 25 May 2026 12:36:48 |
| Eccentricity: | 0.0003025 |
| inclination: | 81.3016° |
| perigee height: | 943 km |
| apogee height: | 947 km |
| right ascension of ascending node: | 232.5733° |
| argument of perigee: | 253.5941° |
| revolutions per day: | 13.85300692 |
| mean anomaly at epoch: | 106.4884° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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