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 42832U 26150.41554782 +.00000000 +00000-0 +35866-3 0 00003
2 42832 97.4142 311.6022 0010489 166.1599 193.9919 15.07980816 08
| Epoch (UTC): | 30 May 2026 09:58:23 |
| Eccentricity: | 0.0010489 |
| inclination: | 97.4142° |
| perigee height: | 535 km |
| apogee height: | 550 km |
| right ascension of ascending node: | 311.6022° |
| argument of perigee: | 166.1599° |
| revolutions per day: | 15.07980816 |
| mean anomaly at epoch: | 193.9919° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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