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 31793U 26088.21880494 +.00000000 +00000-0 +35730-4 0 00008
2 31793 70.9747 131.3347 0002734 277.8941 145.2253 14.14843564 07
| Epoch (UTC): | 29 March 2026 05:15:04 |
| Eccentricity: | 0.0002734 |
| inclination: | 70.9747° |
| perigee height: | 841 km |
| apogee height: | 845 km |
| right ascension of ascending node: | 131.3347° |
| argument of perigee: | 277.8941° |
| revolutions per day: | 14.14843564 |
| mean anomaly at epoch: | 145.2253° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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