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 62487U 26137.03706066 +.00000000 +00000-0 +37758-3 0 00000
2 62487 43.0033 263.0555 0001002 257.3059 102.7681 15.27587135 01
| Epoch (UTC): | 17 May 2026 00:53:22 |
| Eccentricity: | 0.0001002 |
| inclination: | 43.0033° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 263.0555° |
| argument of perigee: | 257.3059° |
| revolutions per day: | 15.27587135 |
| mean anomaly at epoch: | 102.7681° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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