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 53660U 26145.60749135 +.00000000 +00000-0 -31231-4 0 00001
2 53660 97.4518 25.5765 0002491 71.3981 288.7516 15.05655143 03
| Epoch (UTC): | 25 May 2026 14:34:47 |
| Eccentricity: | 0.0002491 |
| inclination: | 97.4518° |
| perigee height: | 548 km |
| apogee height: | 551 km |
| right ascension of ascending node: | 25.5765° |
| argument of perigee: | 71.3981° |
| revolutions per day: | 15.05655143 |
| mean anomaly at epoch: | 288.7516° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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