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 66925U 26145.33752014 +.00000000 +00000-0 +87877-3 0 00004
2 66925 53.1609 2.2975 0001478 94.7569 265.3602 15.34408183 00
| Epoch (UTC): | 25 May 2026 08:06:01 |
| Eccentricity: | 0.0001478 |
| inclination: | 53.1609° |
| perigee height: | 462 km |
| apogee height: | 464 km |
| right ascension of ascending node: | 2.2975° |
| argument of perigee: | 94.7569° |
| revolutions per day: | 15.34408183 |
| mean anomaly at epoch: | 265.3602° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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