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 66303U 26145.56784144 +.00000000 +00000-0 +20896-3 0 00006
2 66303 45.4007 241.7563 0007001 274.1439 85.8648 15.21036879 07
| Epoch (UTC): | 25 May 2026 13:37:41 |
| Eccentricity: | 0.0007001 |
| inclination: | 45.4007° |
| perigee height: | 498 km |
| apogee height: | 508 km |
| right ascension of ascending node: | 241.7563° |
| argument of perigee: | 274.1439° |
| revolutions per day: | 15.21036879 |
| mean anomaly at epoch: | 85.8648° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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