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 26017.30333925 +.00000000 +00000-0 +38580-3 0 00001
2 28737 97.7452 43.4922 0016239 190.1717 169.9190 15.18864865 01
| Epoch (UTC): | 17 January 2026 07:16:48 |
| Eccentricity: | 0.0016239 |
| inclination: | 97.7452° |
| perigee height: | 498 km |
| apogee height: | 520 km |
| right ascension of ascending node: | 43.4922° |
| argument of perigee: | 190.1717° |
| revolutions per day: | 15.18864865 |
| mean anomaly at epoch: | 169.9190° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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