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 10095U 26088.13604280 +.00000000 +00000-0 +78141-4 0 00001
2 10095 75.8328 331.9330 0035980 190.9647 169.0768 14.96640018 09
| Epoch (UTC): | 29 March 2026 03:15:54 |
| Eccentricity: | 0.0035980 |
| inclination: | 75.8328° |
| perigee height: | 552 km |
| apogee height: | 602 km |
| right ascension of ascending node: | 331.9330° |
| argument of perigee: | 190.9647° |
| revolutions per day: | 14.96640018 |
| mean anomaly at epoch: | 169.0768° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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