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 63092U 26145.45522973 +.00000000 +00000-0 +21018-3 0 00003
2 63092 70.0001 160.7886 0004092 266.2297 93.8394 14.98334001 04
| Epoch (UTC): | 25 May 2026 10:55:31 |
| Eccentricity: | 0.0004092 |
| inclination: | 70.0001° |
| perigee height: | 569 km |
| apogee height: | 575 km |
| right ascension of ascending node: | 160.7886° |
| argument of perigee: | 266.2297° |
| revolutions per day: | 14.98334001 |
| mean anomaly at epoch: | 93.8394° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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