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 28773U 05025A 25005.15908413 .07119502 -34455-5 81708-3 0 9991
2 28773 31.3669 169.3333 0002388 343.8481 175.4418 16.35702245 78669
| Epoch (UTC): | 05 January 2025 03:49:04 |
| Eccentricity: | 0.0002388 |
| inclination: | 31.3669° |
| perigee height: | 176 km |
| apogee height: | 179 km |
| right ascension of ascending node: | 169.3333° |
| argument of perigee: | 343.8481° |
| revolutions per day: | 16.35702245 |
| mean anomaly at epoch: | 175.4418° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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