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 62808U 26144.85141402 +.00000000 +00000-0 +72285-3 0 00006
2 62808 53.1601 315.5128 0000660 105.4138 254.6937 15.31713687 09
| Epoch (UTC): | 24 May 2026 20:26:02 |
| Eccentricity: | 0.0000660 |
| inclination: | 53.1601° |
| perigee height: | 470 km |
| apogee height: | 471 km |
| right ascension of ascending node: | 315.5128° |
| argument of perigee: | 105.4138° |
| revolutions per day: | 15.31713687 |
| mean anomaly at epoch: | 254.6937° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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