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 42794U 26087.86422624 +.00000000 +00000-0 +51806-3 0 00009
2 42794 97.5503 67.0871 0085633 80.2860 280.8032 15.15858607 04
| Epoch (UTC): | 28 March 2026 20:44:29 |
| Eccentricity: | 0.0085633 |
| inclination: | 97.5503° |
| perigee height: | 459 km |
| apogee height: | 577 km |
| right ascension of ascending node: | 67.0871° |
| argument of perigee: | 80.2860° |
| revolutions per day: | 15.15858607 |
| mean anomaly at epoch: | 280.8032° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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