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 66454U 26145.56812837 +.00000000 +00000-0 +00000-0 0 00006
2 66454 0.0273 188.5236 0000561 243.4910 296.6993 1.00271399 03
| Epoch (UTC): | 25 May 2026 13:38:06 |
| Eccentricity: | 0.0000561 |
| inclination: | 0.0273° |
| perigee height: | 35784 km |
| apogee height: | 35789 km |
| right ascension of ascending node: | 188.5236° |
| argument of perigee: | 243.4910° |
| revolutions per day: | 1.00271399 |
| mean anomaly at epoch: | 296.6993° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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