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 26076.22888455 +.00000000 +00000-0 +17303-3 0 00001
2 25876 51.7613 271.1652 0502553 10.6705 350.4432 14.11859475 02
| Epoch (UTC): | 17 March 2026 05:29:35 |
| Eccentricity: | 0.0502553 |
| inclination: | 51.7613° |
| perigee height: | 490 km |
| apogee height: | 1216 km |
| right ascension of ascending node: | 271.1652° |
| argument of perigee: | 10.6705° |
| revolutions per day: | 14.11859475 |
| mean anomaly at epoch: | 350.4432° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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