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 59809U 26145.10453330 +.00000000 +00000-0 +52092-3 0 00002
2 59809 97.6537 277.0260 0006970 223.3624 136.7072 15.35698449 08
| Epoch (UTC): | 25 May 2026 02:30:31 |
| Eccentricity: | 0.0006970 |
| inclination: | 97.6537° |
| perigee height: | 454 km |
| apogee height: | 464 km |
| right ascension of ascending node: | 277.0260° |
| argument of perigee: | 223.3624° |
| revolutions per day: | 15.35698449 |
| mean anomaly at epoch: | 136.7072° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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