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 59431U 26145.38986321 +.00000000 +00000-0 +46778-4 0 00009
2 59431 53.1618 285.3344 0001259 84.5938 275.5206 15.30196144 02
| Epoch (UTC): | 25 May 2026 09:21:24 |
| Eccentricity: | 0.0001259 |
| inclination: | 53.1618° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 285.3344° |
| argument of perigee: | 84.5938° |
| revolutions per day: | 15.30196144 |
| mean anomaly at epoch: | 275.5206° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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