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 65699U 26145.59497161 +.00000000 +00000-0 +46899-3 0 00007
2 65699 53.1586 348.7706 0000742 36.5432 323.5620 15.30200403 05
| Epoch (UTC): | 25 May 2026 14:16:45 |
| Eccentricity: | 0.0000742 |
| inclination: | 53.1586° |
| perigee height: | 475 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 348.7706° |
| argument of perigee: | 36.5432° |
| revolutions per day: | 15.30200403 |
| mean anomaly at epoch: | 323.5620° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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