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 62682U 26145.19446578 +.00000000 +00000-0 +22810-3 0 00005
2 62682 97.3905 224.9643 0006436 74.1720 286.0226 15.24457051 09
| Epoch (UTC): | 25 May 2026 04:40:01 |
| Eccentricity: | 0.0006436 |
| inclination: | 97.3905° |
| perigee height: | 488 km |
| apogee height: | 497 km |
| right ascension of ascending node: | 224.9643° |
| argument of perigee: | 74.1720° |
| revolutions per day: | 15.24457051 |
| mean anomaly at epoch: | 286.0226° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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