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 26067.94622068 +.00000000 +00000-0 +26052-3 0 00007
2 25876 51.7627 304.2503 0502372 346.2414 12.5237 14.11835757 00
| Epoch (UTC): | 08 March 2026 22:42:33 |
| Eccentricity: | 0.0502372 |
| inclination: | 51.7627° |
| perigee height: | 490 km |
| apogee height: | 1216 km |
| right ascension of ascending node: | 304.2503° |
| argument of perigee: | 346.2414° |
| revolutions per day: | 14.11835757 |
| mean anomaly at epoch: | 12.5237° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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