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 65637U 26145.17167861 +.00000000 +00000-0 +67648-3 0 00009
2 65637 53.1607 310.9199 0001065 97.0380 263.0744 15.34405714 02
| Epoch (UTC): | 25 May 2026 04:07:13 |
| Eccentricity: | 0.0001065 |
| inclination: | 53.1607° |
| perigee height: | 462 km |
| apogee height: | 463 km |
| right ascension of ascending node: | 310.9199° |
| argument of perigee: | 97.0380° |
| revolutions per day: | 15.34405714 |
| mean anomaly at epoch: | 263.0744° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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