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 39771U 26100.40787661 +.00000000 +00000-0 +33000-3 0 00007
2 39771 98.1977 91.4312 0009466 28.5274 331.6472 15.13963927 05
| Epoch (UTC): | 10 April 2026 09:47:20 |
| Eccentricity: | 0.0009466 |
| inclination: | 98.1977° |
| perigee height: | 518 km |
| apogee height: | 531 km |
| right ascension of ascending node: | 91.4312° |
| argument of perigee: | 28.5274° |
| revolutions per day: | 15.13963927 |
| mean anomaly at epoch: | 331.6472° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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