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 10676U 26087.99629280 +.00000000 +00000-0 +57435-4 0 00009
2 10676 74.0375 298.5223 0017254 289.4734 70.4555 14.37220217 00
| Epoch (UTC): | 28 March 2026 23:54:39 |
| Eccentricity: | 0.0017254 |
| inclination: | 74.0375° |
| perigee height: | 755 km |
| apogee height: | 780 km |
| right ascension of ascending node: | 298.5223° |
| argument of perigee: | 289.4734° |
| revolutions per day: | 14.37220217 |
| mean anomaly at epoch: | 70.4555° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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