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 26072.90167897 +.00000000 +00000-0 +26070-3 0 00003
2 25876 51.7621 284.4563 0502476 0.8549 359.3133 14.11851718 08
| Epoch (UTC): | 13 March 2026 21:38:25 |
| Eccentricity: | 0.0502476 |
| inclination: | 51.7621° |
| perigee height: | 490 km |
| apogee height: | 1216 km |
| right ascension of ascending node: | 284.4563° |
| argument of perigee: | 0.8549° |
| revolutions per day: | 14.11851718 |
| mean anomaly at epoch: | 359.3133° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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