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 26094U 26148.98609185 +.00000000 +00000-0 +21266-3 0 00001
2 26094 100.2167 162.0983 0030985 239.2747 120.5386 14.47267335 05
| Epoch (UTC): | 28 May 2026 23:39:58 |
| Eccentricity: | 0.0030985 |
| inclination: | 100.2167° |
| perigee height: | 713 km |
| apogee height: | 757 km |
| right ascension of ascending node: | 162.0983° |
| argument of perigee: | 239.2747° |
| revolutions per day: | 14.47267335 |
| mean anomaly at epoch: | 120.5386° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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