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 42833U 26150.42046456 +.00000000 +00000-0 +36527-3 0 00004
2 42833 97.4330 313.8660 0007191 148.0642 212.1024 15.08974320 09
| Epoch (UTC): | 30 May 2026 10:05:28 |
| Eccentricity: | 0.0007191 |
| inclination: | 97.4330° |
| perigee height: | 534 km |
| apogee height: | 544 km |
| right ascension of ascending node: | 313.8660° |
| argument of perigee: | 148.0642° |
| revolutions per day: | 15.08974320 |
| mean anomaly at epoch: | 212.1024° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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