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 28894U 26106.65791372 +.00000000 +00000-0 +67850-4 0 00009
2 28894 98.2976 246.0270 0017117 111.1119 249.1915 14.65311282 01
| Epoch (UTC): | 16 April 2026 15:47:23 |
| Eccentricity: | 0.0017117 |
| inclination: | 98.2976° |
| perigee height: | 664 km |
| apogee height: | 688 km |
| right ascension of ascending node: | 246.0270° |
| argument of perigee: | 111.1119° |
| revolutions per day: | 14.65311282 |
| mean anomaly at epoch: | 249.1915° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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