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 58880U 26145.17080580 +.00000000 +00000-0 +17766-3 0 00009
2 58880 53.1609 311.9630 0000944 94.3512 265.7597 15.30202651 05
| Epoch (UTC): | 25 May 2026 04:05:57 |
| Eccentricity: | 0.0000944 |
| inclination: | 53.1609° |
| perigee height: | 475 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 311.9630° |
| argument of perigee: | 94.3512° |
| revolutions per day: | 15.30202651 |
| mean anomaly at epoch: | 265.7597° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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