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 66221U 26145.53295332 +.00000000 +00000-0 +16712-3 0 00000
2 66221 53.1575 233.0471 0001068 87.5445 272.5678 15.30196931 08
| Epoch (UTC): | 25 May 2026 12:47:27 |
| Eccentricity: | 0.0001068 |
| inclination: | 53.1575° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 233.0471° |
| argument of perigee: | 87.5445° |
| revolutions per day: | 15.30196931 |
| mean anomaly at epoch: | 272.5678° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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