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 65659U 26145.53426779 +.00000000 +00000-0 +22943-3 0 00008
2 65659 97.4465 189.4186 0001053 122.2774 237.8555 15.05655148 04
| Epoch (UTC): | 25 May 2026 12:49:20 |
| Eccentricity: | 0.0001053 |
| inclination: | 97.4465° |
| perigee height: | 549 km |
| apogee height: | 550 km |
| right ascension of ascending node: | 189.4186° |
| argument of perigee: | 122.2774° |
| revolutions per day: | 15.05655148 |
| mean anomaly at epoch: | 237.8555° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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