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 26062.75918865 +.00000000 +00000-0 +00000-0 0 00001
2 42692 0.0203 115.2730 0002766 241.1092 3.5813 1.00271776 00
| Epoch (UTC): | 03 March 2026 18:13:13 |
| Eccentricity: | 0.0002766 |
| inclination: | 0.0203° |
| perigee height: | 35775 km |
| apogee height: | 35798 km |
| right ascension of ascending node: | 115.2730° |
| argument of perigee: | 241.1092° |
| revolutions per day: | 1.00271776 |
| mean anomaly at epoch: | 3.5813° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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