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 42829U 26145.37591098 +.00000000 +00000-0 +23269-3 0 00003
2 42829 97.4268 303.9083 0018167 167.1884 192.9808 15.04797923 01
| Epoch (UTC): | 25 May 2026 09:01:18 |
| Eccentricity: | 0.0018167 |
| inclination: | 97.4268° |
| perigee height: | 540 km |
| apogee height: | 565 km |
| right ascension of ascending node: | 303.9083° |
| argument of perigee: | 167.1884° |
| revolutions per day: | 15.04797923 |
| mean anomaly at epoch: | 192.9808° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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