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 26094U 26157.76605469 +.00000000 +00000-0 +20538-3 0 00009
2 26094 100.2164 172.6823 0031280 213.6430 146.2771 14.47281848 04
| Epoch (UTC): | 06 June 2026 18:23:07 |
| Eccentricity: | 0.0031280 |
| inclination: | 100.2164° |
| perigee height: | 712 km |
| apogee height: | 757 km |
| right ascension of ascending node: | 172.6823° |
| argument of perigee: | 213.6430° |
| revolutions per day: | 14.47281848 |
| mean anomaly at epoch: | 146.2771° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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