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 51733U 26145.50998707 +.00000000 +00000-0 +12858-3 0 00002
2 51733 53.2115 334.2711 0001280 78.9869 281.1267 15.08830000 09
| Epoch (UTC): | 25 May 2026 12:14:22 |
| Eccentricity: | 0.0001280 |
| inclination: | 53.2115° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 334.2711° |
| argument of perigee: | 78.9869° |
| revolutions per day: | 15.08830000 |
| mean anomaly at epoch: | 281.1267° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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