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 66158U 26145.47506024 +.00000000 +00000-0 +82313-3 0 00005
2 66158 53.1577 66.2214 0001004 81.0136 279.0978 15.30209891 01
| Epoch (UTC): | 25 May 2026 11:24:05 |
| Eccentricity: | 0.0001004 |
| inclination: | 53.1577° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 66.2214° |
| argument of perigee: | 81.0136° |
| revolutions per day: | 15.30209891 |
| mean anomaly at epoch: | 279.0978° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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