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 26042.03575242 +.00000000 +00000-0 +38874-3 0 00006
2 25876 51.7656 47.7203 0502271 269.6917 84.6473 14.11731071 08
| Epoch (UTC): | 11 February 2026 00:51:29 |
| Eccentricity: | 0.0502271 |
| inclination: | 51.7656° |
| perigee height: | 490 km |
| apogee height: | 1217 km |
| right ascension of ascending node: | 47.7203° |
| argument of perigee: | 269.6917° |
| revolutions per day: | 14.11731071 |
| mean anomaly at epoch: | 84.6473° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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