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 00728U 26088.17290975 +.00000000 +00000-0 +93576-4 0 00008
2 00728 69.9102 15.8965 0010586 90.8448 269.3871 13.97759246 02
| Epoch (UTC): | 29 March 2026 04:08:59 |
| Eccentricity: | 0.0010586 |
| inclination: | 69.9102° |
| perigee height: | 894 km |
| apogee height: | 909 km |
| right ascension of ascending node: | 15.8965° |
| argument of perigee: | 90.8448° |
| revolutions per day: | 13.97759246 |
| mean anomaly at epoch: | 269.3871° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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