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 28059U 26041.90772008 +.00000000 +00000-0 +13827-3 0 00007
2 28059 98.6850 35.7683 0047355 314.5123 45.2207 14.54990791 06
| Epoch (UTC): | 10 February 2026 21:47:07 |
| Eccentricity: | 0.0047355 |
| inclination: | 98.6850° |
| perigee height: | 676 km |
| apogee height: | 743 km |
| right ascension of ascending node: | 35.7683° |
| argument of perigee: | 314.5123° |
| revolutions per day: | 14.54990791 |
| mean anomaly at epoch: | 45.2207° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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