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 42692U 26107.63641845 +.00000000 +00000-0 +00000-0 0 00009
2 42692 0.0511 67.2866 0002754 333.6350 319.1079 1.00270738 06
| Epoch (UTC): | 17 April 2026 15:16:26 |
| Eccentricity: | 0.0002754 |
| inclination: | 0.0511° |
| perigee height: | 35775 km |
| apogee height: | 35799 km |
| right ascension of ascending node: | 67.2866° |
| argument of perigee: | 333.6350° |
| revolutions per day: | 1.00270738 |
| mean anomaly at epoch: | 319.1079° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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