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 26069.00810878 +.00000000 +00000-0 +24629-3 0 00002
2 25876 51.7624 300.0088 0502409 349.3726 9.6894 14.11838777 01
| Epoch (UTC): | 10 March 2026 00:11:40 |
| Eccentricity: | 0.0502409 |
| inclination: | 51.7624° |
| perigee height: | 490 km |
| apogee height: | 1216 km |
| right ascension of ascending node: | 300.0088° |
| argument of perigee: | 349.3726° |
| revolutions per day: | 14.11838777 |
| mean anomaly at epoch: | 9.6894° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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