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 66069U 26145.56672995 +.00000000 +00000-0 +11928-2 0 00000
2 66069 53.1588 248.0431 0001123 103.6051 256.5075 15.30220281 08
| Epoch (UTC): | 25 May 2026 13:36:05 |
| Eccentricity: | 0.0001123 |
| inclination: | 53.1588° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 248.0431° |
| argument of perigee: | 103.6051° |
| revolutions per day: | 15.30220281 |
| mean anomaly at epoch: | 256.5075° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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