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 57982U 26145.64187080 +.00000000 +00000-0 +39313-4 0 00009
2 57982 43.0028 279.3807 0001993 269.5459 90.5164 15.27573436 06
| Epoch (UTC): | 25 May 2026 15:24:17 |
| Eccentricity: | 0.0001993 |
| inclination: | 43.0028° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 279.3807° |
| argument of perigee: | 269.5459° |
| revolutions per day: | 15.27573436 |
| mean anomaly at epoch: | 90.5164° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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