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 42844U 26150.43885796 +.00000000 +00000-0 +70220-3 0 00003
2 42844 97.3727 325.0086 0005548 84.2642 275.9227 15.24095754 07
| Epoch (UTC): | 30 May 2026 10:31:57 |
| Eccentricity: | 0.0005548 |
| inclination: | 97.3727° |
| perigee height: | 490 km |
| apogee height: | 497 km |
| right ascension of ascending node: | 325.0086° |
| argument of perigee: | 84.2642° |
| revolutions per day: | 15.24095754 |
| mean anomaly at epoch: | 275.9227° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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