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 65451U 26145.55309501 +.00000000 +00000-0 +23234-3 0 00007
2 65451 97.4532 359.7698 0002090 80.3116 279.8347 15.05655159 02
| Epoch (UTC): | 25 May 2026 13:16:27 |
| Eccentricity: | 0.0002090 |
| inclination: | 97.4532° |
| perigee height: | 548 km |
| apogee height: | 551 km |
| right ascension of ascending node: | 359.7698° |
| argument of perigee: | 80.3116° |
| revolutions per day: | 15.05655159 |
| mean anomaly at epoch: | 279.8347° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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