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 58130U 26145.11366024 +.00000000 +00000-0 +33053-4 0 00009
2 58130 43.0018 57.6075 0000976 271.7997 88.2743 15.27581848 00
| Epoch (UTC): | 25 May 2026 02:43:40 |
| Eccentricity: | 0.0000976 |
| inclination: | 43.0018° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 57.6075° |
| argument of perigee: | 271.7997° |
| revolutions per day: | 15.27581848 |
| mean anomaly at epoch: | 88.2743° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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