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 35681U 26145.59978882 +.00000000 +00000-0 +73456-4 0 00009
2 35681 97.7382 303.8102 0000210 94.9013 265.2221 14.75209091 05
| Epoch (UTC): | 25 May 2026 14:23:41 |
| Eccentricity: | 0.0000210 |
| inclination: | 97.7382° |
| perigee height: | 644 km |
| apogee height: | 645 km |
| right ascension of ascending node: | 303.8102° |
| argument of perigee: | 94.9013° |
| revolutions per day: | 14.75209091 |
| mean anomaly at epoch: | 265.2221° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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