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 66305U 26145.54868538 +.00000000 +00000-0 +57864-3 0 00001
2 66305 45.4198 236.0236 0013102 285.6421 74.3023 15.27036385 09
| Epoch (UTC): | 25 May 2026 13:10:06 |
| Eccentricity: | 0.0013102 |
| inclination: | 45.4198° |
| perigee height: | 476 km |
| apogee height: | 494 km |
| right ascension of ascending node: | 236.0236° |
| argument of perigee: | 285.6421° |
| revolutions per day: | 15.27036385 |
| mean anomaly at epoch: | 74.3023° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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