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 42831U 26145.58734962 +.00000000 +00000-0 +27890-3 0 00002
2 42831 97.4590 302.0063 0018277 197.2979 162.7625 15.00975583 09
| Epoch (UTC): | 25 May 2026 14:05:47 |
| Eccentricity: | 0.0018277 |
| inclination: | 97.4590° |
| perigee height: | 551 km |
| apogee height: | 577 km |
| right ascension of ascending node: | 302.0063° |
| argument of perigee: | 197.2979° |
| revolutions per day: | 15.00975583 |
| mean anomaly at epoch: | 162.7625° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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