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 44723U 26145.49078624 +.00000000 +00000-0 +10683-2 0 00001
2 44723 53.0476 175.3088 0005345 354.1847 5.9090 15.30256417 05
| Epoch (UTC): | 25 May 2026 11:46:43 |
| Eccentricity: | 0.0005345 |
| inclination: | 53.0476° |
| perigee height: | 471 km |
| apogee height: | 479 km |
| right ascension of ascending node: | 175.3088° |
| argument of perigee: | 354.1847° |
| revolutions per day: | 15.30256417 |
| mean anomaly at epoch: | 5.9090° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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