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 26366U 26071.73030262 +.00000000 +00000-0 +11324-3 0 00009
2 26366 86.3512 175.0129 0003605 269.5096 90.5739 15.29057295 04
| Epoch (UTC): | 12 March 2026 17:31:38 |
| Eccentricity: | 0.0003605 |
| inclination: | 86.3512° |
| perigee height: | 476 km |
| apogee height: | 481 km |
| right ascension of ascending node: | 175.0129° |
| argument of perigee: | 269.5096° |
| revolutions per day: | 15.29057295 |
| mean anomaly at epoch: | 90.5739° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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