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 26075.05601968 +.00000000 +00000-0 +38644-3 0 00003
2 28737 97.7396 102.7068 0016029 2.1201 358.0098 15.20096104 09
| Epoch (UTC): | 16 March 2026 01:20:40 |
| Eccentricity: | 0.0016029 |
| inclination: | 97.7396° |
| perigee height: | 495 km |
| apogee height: | 517 km |
| right ascension of ascending node: | 102.7068° |
| argument of perigee: | 2.1201° |
| revolutions per day: | 15.20096104 |
| mean anomaly at epoch: | 358.0098° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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