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 40261U 26145.60902670 +.00000000 +00000-0 +10219-3 0 00000
2 40261 97.9944 215.5739 0009734 215.1801 144.8760 14.63711993 04
| Epoch (UTC): | 25 May 2026 14:36:59 |
| Eccentricity: | 0.0009734 |
| inclination: | 97.9944° |
| perigee height: | 674 km |
| apogee height: | 688 km |
| right ascension of ascending node: | 215.5739° |
| argument of perigee: | 215.1801° |
| revolutions per day: | 14.63711993 |
| mean anomaly at epoch: | 144.8760° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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