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 26071.63294606 +.00000000 +00000-0 +43865-3 0 00001
2 28737 97.7409 99.1956 0016380 13.8076 346.3603 15.20026822 00
| Epoch (UTC): | 12 March 2026 15:11:26 |
| Eccentricity: | 0.0016380 |
| inclination: | 97.7409° |
| perigee height: | 494 km |
| apogee height: | 517 km |
| right ascension of ascending node: | 99.1956° |
| argument of perigee: | 13.8076° |
| revolutions per day: | 15.20026822 |
| mean anomaly at epoch: | 346.3603° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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