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 60292U 26145.58335647 +.00000000 +00000-0 +17118-2 0 00001
2 60292 53.1606 55.4113 0001227 92.8315 176.7419 15.31669277 03
| Epoch (UTC): | 25 May 2026 14:00:01 |
| Eccentricity: | 0.0001227 |
| inclination: | 53.1606° |
| perigee height: | 470 km |
| apogee height: | 472 km |
| right ascension of ascending node: | 55.4113° |
| argument of perigee: | 92.8315° |
| revolutions per day: | 15.31669277 |
| mean anomaly at epoch: | 176.7419° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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