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 58326U 26145.60351634 +.00000000 +00000-0 +43072-3 0 00002
2 58326 97.3794 230.5642 0004868 228.8131 131.2699 15.45054153 02
| Epoch (UTC): | 25 May 2026 14:29:03 |
| Eccentricity: | 0.0004868 |
| inclination: | 97.3794° |
| perigee height: | 428 km |
| apogee height: | 435 km |
| right ascension of ascending node: | 230.5642° |
| argument of perigee: | 228.8131° |
| revolutions per day: | 15.45054153 |
| mean anomaly at epoch: | 131.2699° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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