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 25991U 26053.86554397 +.00000000 +00000-0 +88389-4 0 00002
2 25991 99.0124 90.9148 0009358 333.4619 26.2615 14.17513335 03
| Epoch (UTC): | 22 February 2026 20:46:22 |
| Eccentricity: | 0.0009358 |
| inclination: | 99.0124° |
| perigee height: | 827 km |
| apogee height: | 841 km |
| right ascension of ascending node: | 90.9148° |
| argument of perigee: | 333.4619° |
| revolutions per day: | 14.17513335 |
| mean anomaly at epoch: | 26.2615° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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