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 58894U 26145.51201080 +.00000000 +00000-0 +34934-4 0 00009
2 58894 53.1611 325.5372 0001180 91.0218 269.0919 15.31704500 03
| Epoch (UTC): | 25 May 2026 12:17:17 |
| Eccentricity: | 0.0001180 |
| inclination: | 53.1611° |
| perigee height: | 470 km |
| apogee height: | 472 km |
| right ascension of ascending node: | 325.5372° |
| argument of perigee: | 91.0218° |
| revolutions per day: | 15.31704500 |
| mean anomaly at epoch: | 269.0919° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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