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 59261U 26145.39009087 +.00000000 +00000-0 +26711-4 0 00001
2 59261 53.1596 184.5966 0000582 63.8023 296.3037 15.30192661 04
| Epoch (UTC): | 25 May 2026 09:21:43 |
| Eccentricity: | 0.0000582 |
| inclination: | 53.1596° |
| perigee height: | 475 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 184.5966° |
| argument of perigee: | 63.8023° |
| revolutions per day: | 15.30192661 |
| mean anomaly at epoch: | 296.3037° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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