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 42842U 26145.47050721 +.00000000 +00000-0 +56665-3 0 00008
2 42842 97.3826 327.2272 0008148 99.8503 260.3658 15.29498732 07
| Epoch (UTC): | 25 May 2026 11:17:31 |
| Eccentricity: | 0.0008148 |
| inclination: | 97.3826° |
| perigee height: | 472 km |
| apogee height: | 483 km |
| right ascension of ascending node: | 327.2272° |
| argument of perigee: | 99.8503° |
| revolutions per day: | 15.29498732 |
| mean anomaly at epoch: | 260.3658° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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