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 42695U 26106.95989608 +.00000000 +00000-0 +00000-0 0 00008
2 42695 0.0263 35.6994 0002867 343.6980 268.5758 1.00270199 01
| Epoch (UTC): | 16 April 2026 23:02:15 |
| Eccentricity: | 0.0002867 |
| inclination: | 0.0263° |
| perigee height: | 35775 km |
| apogee height: | 35799 km |
| right ascension of ascending node: | 35.6994° |
| argument of perigee: | 343.6980° |
| revolutions per day: | 1.00270199 |
| mean anomaly at epoch: | 268.5758° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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