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 31081U 26107.78935795 +.00000000 +00000-0 +14528-3 0 00008
2 31081 98.7632 125.2723 0047259 236.5565 301.5887 14.06325854 01
| Epoch (UTC): | 17 April 2026 18:56:40 |
| Eccentricity: | 0.0047259 |
| inclination: | 98.7632° |
| perigee height: | 838 km |
| apogee height: | 906 km |
| right ascension of ascending node: | 125.2723° |
| argument of perigee: | 236.5565° |
| revolutions per day: | 14.06325854 |
| mean anomaly at epoch: | 301.5887° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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