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 39768U 26088.16747749 +.00000000 +00000-0 +29067-3 0 00002
2 39768 97.8967 201.0694 0005129 238.5487 121.5231 14.94464713 05
| Epoch (UTC): | 29 March 2026 04:01:10 |
| Eccentricity: | 0.0005129 |
| inclination: | 97.8967° |
| perigee height: | 580 km |
| apogee height: | 588 km |
| right ascension of ascending node: | 201.0694° |
| argument of perigee: | 238.5487° |
| revolutions per day: | 14.94464713 |
| mean anomaly at epoch: | 121.5231° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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