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 42698U 26145.59490847 +.00000000 +00000-0 +00000-0 0 00006
2 42698 0.0178 335.0288 0000303 69.4980 109.3217 1.00272582 08
| Epoch (UTC): | 25 May 2026 14:16:40 |
| Eccentricity: | 0.0000303 |
| inclination: | 0.0178° |
| perigee height: | 35785 km |
| apogee height: | 35788 km |
| right ascension of ascending node: | 335.0288° |
| argument of perigee: | 69.4980° |
| revolutions per day: | 1.00272582 |
| mean anomaly at epoch: | 109.3217° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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