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 26106.67445808 +.00000000 +00000-0 +30056-3 0 00003
2 42794 97.5524 85.8044 0083529 16.3344 344.0550 15.16246037 03
| Epoch (UTC): | 16 April 2026 16:11:13 |
| Eccentricity: | 0.0083529 |
| inclination: | 97.5524° |
| perigee height: | 460 km |
| apogee height: | 575 km |
| right ascension of ascending node: | 85.8044° |
| argument of perigee: | 16.3344° |
| revolutions per day: | 15.16246037 |
| mean anomaly at epoch: | 344.0550° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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