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 62871U 26145.39840899 +.00000000 +00000-0 +52700-3 0 00002
2 62871 53.1569 133.3791 0001173 92.9282 267.1853 15.30210826 06
| Epoch (UTC): | 25 May 2026 09:33:42 |
| Eccentricity: | 0.0001173 |
| inclination: | 53.1569° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 133.3791° |
| argument of perigee: | 92.9282° |
| revolutions per day: | 15.30210826 |
| mean anomaly at epoch: | 267.1853° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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