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 58648U 26145.62599380 +.00000000 +00000-0 +20362-3 0 00000
2 58648 97.3414 166.7698 0009406 60.3931 299.8244 15.26578111 00
| Epoch (UTC): | 25 May 2026 15:01:25 |
| Eccentricity: | 0.0009406 |
| inclination: | 97.3414° |
| perigee height: | 480 km |
| apogee height: | 493 km |
| right ascension of ascending node: | 166.7698° |
| argument of perigee: | 60.3931° |
| revolutions per day: | 15.26578111 |
| mean anomaly at epoch: | 299.8244° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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