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 42810U 26145.38120514 +.00000000 +00000-0 -83909-5 0 00005
2 42810 86.4458 299.8991 0002072 91.1231 269.0208 14.43279801 03
| Epoch (UTC): | 25 May 2026 09:08:56 |
| Eccentricity: | 0.0002072 |
| inclination: | 86.4458° |
| perigee height: | 746 km |
| apogee height: | 749 km |
| right ascension of ascending node: | 299.8991° |
| argument of perigee: | 91.1231° |
| revolutions per day: | 14.43279801 |
| mean anomaly at epoch: | 269.0208° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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