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 58467U 26145.52103895 +.00000000 +00000-0 +13129-2 0 00002
2 58467 97.3217 229.2368 0010771 238.7279 121.2947 16.03421006 06
| Epoch (UTC): | 25 May 2026 12:30:17 |
| Eccentricity: | 0.0010771 |
| inclination: | 97.3217° |
| perigee height: | 258 km |
| apogee height: | 272 km |
| right ascension of ascending node: | 229.2368° |
| argument of perigee: | 238.7279° |
| revolutions per day: | 16.03421006 |
| mean anomaly at epoch: | 121.2947° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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