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 25876U 26156.70907516 +.00000000 +00000-0 +14823-3 0 00007
2 25876 51.7659 309.6462 0501036 248.0872 106.6086 14.11994346 08
| Epoch (UTC): | 05 June 2026 17:01:04 |
| Eccentricity: | 0.0501036 |
| inclination: | 51.7659° |
| perigee height: | 490 km |
| apogee height: | 1215 km |
| right ascension of ascending node: | 309.6462° |
| argument of perigee: | 248.0872° |
| revolutions per day: | 14.11994346 |
| mean anomaly at epoch: | 106.6086° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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