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 66258U 26145.39353822 +.00000000 +00000-0 +46226-3 0 00006
2 66258 53.1600 287.3584 0001203 122.8407 237.2710 15.30215566 07
| Epoch (UTC): | 25 May 2026 09:26:41 |
| Eccentricity: | 0.0001203 |
| inclination: | 53.1600° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 287.3584° |
| argument of perigee: | 122.8407° |
| revolutions per day: | 15.30215566 |
| mean anomaly at epoch: | 237.2710° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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