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 66149U 26145.20113632 +.00000000 +00000-0 +92462-3 0 00001
2 66149 53.1580 67.3592 0001188 91.9086 268.2051 15.30208876 07
| Epoch (UTC): | 25 May 2026 04:49:38 |
| Eccentricity: | 0.0001188 |
| inclination: | 53.1580° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 67.3592° |
| argument of perigee: | 91.9086° |
| revolutions per day: | 15.30208876 |
| mean anomaly at epoch: | 268.2051° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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