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 58276U 26145.16474292 +.00000000 +00000-0 +29740-3 0 00009
2 58276 97.3673 223.0269 0005142 262.5357 97.5302 15.34161154 08
| Epoch (UTC): | 25 May 2026 03:57:13 |
| Eccentricity: | 0.0005142 |
| inclination: | 97.3673° |
| perigee height: | 460 km |
| apogee height: | 467 km |
| right ascension of ascending node: | 223.0269° |
| argument of perigee: | 262.5357° |
| revolutions per day: | 15.34161154 |
| mean anomaly at epoch: | 97.5302° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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