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 45044U 26145.27022056 +.00000000 +00000-0 +11102-2 0 00009
2 45044 53.1519 248.2176 0002082 345.9040 14.1912 15.53545360 05
| Epoch (UTC): | 25 May 2026 06:29:07 |
| Eccentricity: | 0.0002082 |
| inclination: | 53.1519° |
| perigee height: | 405 km |
| apogee height: | 408 km |
| right ascension of ascending node: | 248.2176° |
| argument of perigee: | 345.9040° |
| revolutions per day: | 15.53545360 |
| mean anomaly at epoch: | 14.1912° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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