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 58498U 26145.65665904 +.00000000 +00000-0 +15305-3 0 00003
2 58498 97.9291 229.8191 0009987 207.2651 152.8041 14.85734274 07
| Epoch (UTC): | 25 May 2026 15:45:35 |
| Eccentricity: | 0.0009987 |
| inclination: | 97.9291° |
| perigee height: | 604 km |
| apogee height: | 618 km |
| right ascension of ascending node: | 229.8191° |
| argument of perigee: | 207.2651° |
| revolutions per day: | 14.85734274 |
| mean anomaly at epoch: | 152.8041° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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