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 28617U 26087.58923295 +.00000000 +00000-0 +35764-2 0 00000
2 28617 100.4758 318.2479 0046664 260.4459 127.9827 13.80991679 00
| Epoch (UTC): | 28 March 2026 14:08:29 |
| Eccentricity: | 0.0046664 |
| inclination: | 100.4758° |
| perigee height: | 926 km |
| apogee height: | 995 km |
| right ascension of ascending node: | 318.2479° |
| argument of perigee: | 260.4459° |
| revolutions per day: | 13.80991679 |
| mean anomaly at epoch: | 127.9827° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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