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 61580U 26145.40500277 +.00000000 +00000-0 +10474-4 0 00006
2 61580 53.1595 277.7546 0000776 45.1561 314.9520 15.69719309 04
| Epoch (UTC): | 25 May 2026 09:43:12 |
| Eccentricity: | 0.0000776 |
| inclination: | 53.1595° |
| perigee height: | 359 km |
| apogee height: | 360 km |
| right ascension of ascending node: | 277.7546° |
| argument of perigee: | 45.1561° |
| revolutions per day: | 15.69719309 |
| mean anomaly at epoch: | 314.9520° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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