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 35683U 26129.17761402 +.00000000 +00000-0 +29514-4 0 00001
2 35683 97.8781 265.1116 0001677 81.6603 278.4797 14.75965871 01
| Epoch (UTC): | 09 May 2026 04:15:45 |
| Eccentricity: | 0.0001677 |
| inclination: | 97.8781° |
| perigee height: | 641 km |
| apogee height: | 643 km |
| right ascension of ascending node: | 265.1116° |
| argument of perigee: | 81.6603° |
| revolutions per day: | 14.75965871 |
| mean anomaly at epoch: | 278.4797° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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