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 66137U 26144.97090441 +.00000000 +00000-0 +36795-3 0 00000
2 66137 53.1602 45.0040 0001233 102.9825 257.1314 15.30208008 01
| Epoch (UTC): | 24 May 2026 23:18:06 |
| Eccentricity: | 0.0001233 |
| inclination: | 53.1602° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 45.0040° |
| argument of perigee: | 102.9825° |
| revolutions per day: | 15.30208008 |
| mean anomaly at epoch: | 257.1314° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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