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 28737U 26074.59523057 +.00000000 +00000-0 +35637-3 0 00002
2 28737 97.7399 102.2342 0016074 3.8861 356.2495 15.20087434 09
| Epoch (UTC): | 15 March 2026 14:17:07 |
| Eccentricity: | 0.0016074 |
| inclination: | 97.7399° |
| perigee height: | 495 km |
| apogee height: | 517 km |
| right ascension of ascending node: | 102.2342° |
| argument of perigee: | 3.8861° |
| revolutions per day: | 15.20087434 |
| mean anomaly at epoch: | 356.2495° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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