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 66272U 26145.51330051 +.00000000 +00000-0 +40329-3 0 00003
2 66272 53.1584 193.3372 0001237 63.0380 297.0749 15.34401384 03
| Epoch (UTC): | 25 May 2026 12:19:09 |
| Eccentricity: | 0.0001237 |
| inclination: | 53.1584° |
| perigee height: | 462 km |
| apogee height: | 464 km |
| right ascension of ascending node: | 193.3372° |
| argument of perigee: | 63.0380° |
| revolutions per day: | 15.34401384 |
| mean anomaly at epoch: | 297.0749° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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