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 16728U 26075.88820073 +.00000000 +00000-0 +11550-3 0 00008
2 16728 82.9539 127.9617 0029212 262.4137 270.7344 13.77071589 01
| Epoch (UTC): | 16 March 2026 21:19:00 |
| Eccentricity: | 0.0029212 |
| inclination: | 82.9539° |
| perigee height: | 953 km |
| apogee height: | 996 km |
| right ascension of ascending node: | 127.9617° |
| argument of perigee: | 262.4137° |
| revolutions per day: | 13.77071589 |
| mean anomaly at epoch: | 270.7344° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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