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 26069.24338728 +.00000000 +00000-0 +13804-3 0 00005
2 26366 86.3514 176.2343 0003682 285.6253 74.4588 15.29040104 00
| Epoch (UTC): | 10 March 2026 05:50:28 |
| Eccentricity: | 0.0003682 |
| inclination: | 86.3514° |
| perigee height: | 476 km |
| apogee height: | 481 km |
| right ascension of ascending node: | 176.2343° |
| argument of perigee: | 285.6253° |
| revolutions per day: | 15.29040104 |
| mean anomaly at epoch: | 74.4588° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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