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 66735U 26145.17934803 +.00000000 +00000-0 +26685-3 0 00003
2 66735 97.4229 219.1129 0006357 91.3179 268.8784 15.19442204 03
| Epoch (UTC): | 25 May 2026 04:18:15 |
| Eccentricity: | 0.0006357 |
| inclination: | 97.4229° |
| perigee height: | 503 km |
| apogee height: | 512 km |
| right ascension of ascending node: | 219.1129° |
| argument of perigee: | 91.3179° |
| revolutions per day: | 15.19442204 |
| mean anomaly at epoch: | 268.8784° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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